solvay cytec cycom 5320-1 t650 unitape qualification ...page 2 of 317 prepared by: (no longer...

Report No: CAM-RP-2013-002 Rev A Report Date: January 27, 2017

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Solvay Cytec Cycom 5320-1 T650 Unitape Qualification Material Property Data Report

NCAMP Project Number NPN071001

NCAMP Test Report Number: CAM-RP-2013-002 Rev A

Report Date: January 27, 2017 Testing Facility: National Institute for Aviation Research Wichita State University 1845 N. Fairmount Wichita, KS 67260-0093 Test Panel Fabrication Facility: Gulfstream Aerospace Corporation 500 Gulfstream Rd. Savannah, GA 31408

Distribution Statement A. Approved for public release; distribution is unlimited.

Report No: CAM-RP-2013-002 Rev A Report Date: January 27, 2017

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Prepared by: (No longer available to sign) Michelle Man Reviewed by: Royal Lovingfoss Evelyn Lian Approved By: Ed Hooper (NCAMP AER) REVISIONS: Rev By Date Pages Revised or Added

N/C Michelle Man 04/24/2013 Document Initial Release. A Evelyn Lian 1/27/2017 - Editorial corrections for Section 1.1.

- Footnote is added to define ILT layup for Table 2-2.

- Typographical corrections, and deleted empty page deleted for IPS, Section 4.5.

- Added CAI information for Section 5. - Additional Stress vs. Strain charts (LT, TT, TC, UNT, UNC) are added for Section 6. - Typographical/editorial corrections, added

information to categorize the section of Room Temp and Elevated Temp testing) for Section 7.

- Conditioning charts are updated for Section 8. - STDEV is added to DMA results for Section 9.

January 27, 2017 CAM-RP-2013-002 Rev A

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TABLE OF CONTENTS 1. Introduction ................................................................................................................ 8

1.1 Scope ................................................................................................................ 8 1.2 Symbols ............................................................................................................ 9 1.3 NIAR–Specimen Naming Format .................................................................... 11 1.4 References ...................................................................................................... 12 1.5 Methodology ................................................................................................... 13

1.5.1 Process Definition ............................................................................... 13 1.5.2 Specimen & Testing Details ............................................................... 14

1.5.2.1 Tabbing ................................................................................. 14 1.5.2.2 Specimen Dimensions & Test Configuration ......................... 14

1.5.3 Test Matrix .......................................................................................... 15 1.5.4 Cured Laminate Physical Testing ....................................................... 17 1.5.5 Environmental Conditioning ................................................................ 18 1.5.6 Non-ambient Testing .......................................................................... 19 1.5.7 Fluid Sensitivity Screening ................................................................. 19 1.5.8 Normalization Procedures .................................................................. 21 1.5.9 Inspection Verification ........................................................................ 21 1.5.10 Material Pedigree Information ............................................................ 21

2. Test Results ............................................................................................................. 22 2.1 Lamina Level Test Summary .......................................................................... 22 2.2 Laminate Level Test Summary ....................................................................... 23 2.3 Individual Test Summaries .............................................................................. 24

2.3.1 Longitudinal Tension Properties (LT) .................................................. 24 2.3.2 Transverse Tension Properties (TT) ................................................... 25 2.3.3 Longitudinal Compression Properties (LC) ......................................... 26 2.3.4 Transverse Compression Properties (TC) .......................................... 27 2.3.5 In-Plane Shear Properties (IPS) ......................................................... 28 2.3.6 “25/50/25” Unnotched Tension 1 Properties (UNT1) .......................... 29 2.3.7 “10/80/10” Unnotched Tension 2 Properties (UNT2) .......................... 30 2.3.8 “50/40/10” Unnotched Tension 3 Properties (UNT3) .......................... 31 2.3.9 “33/0/67” Unnotched Compression 0 Properties (UNC0) ................... 32 2.3.10 “25/50/25” Unnotched Compression 1 Properties (UNC1) ................. 33 2.3.11 “10/80/10” Unnotched Compression 2 Properties (UNC2) ................. 34 2.3.12 “50/40/10” Unnotched Compression 3 Properties (UNC3) ................. 35 2.3.13 Lamina Short-Beam Strength Properties (SBS) ................................. 36 2.3.14 Laminate Short-Beam Strength Properties (SBS1) ............................ 37 2.3.15 “25/50/25” Open-Hole Tension 1 Properties (OHT1) .......................... 38 2.3.16 “10/80/10” Open-Hole Tension 2 Properties (OHT2) .......................... 39 2.3.17 “50/40/10” Open-Hole Tension 3 Properties (OHT3) .......................... 40 2.3.18 “25/50/25” Filled-Hole Tension 1 Properties (FHT1) ........................... 41 2.3.19 “10/80/10” Filled-Hole Tension 2 Properties (FHT2) ........................... 42 2.3.20 “50/40/10” Filled-Hole Tension 3 Properties (FHT3) ........................... 43 2.3.21 “25/50/25” Open-Hole Compression 1 Properties (OHC1) ................. 44 2.3.22 “10/80/10” Open-Hole Compression 2 Properties (OHC2) ................. 45 2.3.23 “50/40/10” Open-Hole Compression 3 Properties (OHC3) ................. 46


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2.3.24 “25/50/25” Filled-Hole Compression 1 Properties (FHC1) .................. 47 2.3.25 “10/80/10” Filled-Hole Compression 2 Properties (FHC2) .................. 48 2.3.26 “50/40/10” Filled-Hole Compression 3 Properties (FHC3) .................. 49 2.3.27 “25/50/25” Single-Shear Bearing 1 Properties (SSB1) ....................... 50 2.3.28 “10/80/10” Single-Shear Bearing 2 Properties (SSB2) ....................... 51 2.3.29 “50/40/10” Single-Shear Bearing 3 Properties (SSB3) ....................... 52 2.3.30 Compression After Impact 1 Properties (CAI1) .................................. 53 2.3.31 Interlaminar Tension Properties (ILT) ................................................. 54

3. Individual Test Charts .............................................................................................. 55 3.1 Longitudinal Tension Properties (LT) .............................................................. 56 3.2 Transverse Tension Properties (TT) ............................................................... 57 3.3 Longitudinal Compression Properties (LC) ..................................................... 58 3.4 Transverse Compression Properties (TC)....................................................... 59 3.5 In-Plane Shear Properties (IPS) ...................................................................... 60 3.6 “25/50/25” Unnotched Tension 1 Properties (UNT1) ....................................... 62 3.7 “10/80/10” Unnotched Tension 2 Properties (UNT2) ....................................... 63 3.8 “50/40/10” Unnotched Tension 3 Properties (UNT3) ....................................... 64 3.9 “33/0/67” Unnotched Compression 0 Properties (UNC0) ................................ 65 3.10 “25/50/25” Unnotched Compression 1 Properties (UNC1) .............................. 66 3.11 “10/80/10” Unnotched Compression 2 Properties (UNC2) .............................. 67 3.12 “50/40/10” Unnotched Compression 3 Properties (UNC3) .............................. 68 3.13 Lamina Short-Beam Shear Properties (SBS) .................................................. 69 3.14 Laminate Short-Beam Strength Properties (SBS1) ......................................... 69 3.15 “25/50/25” Open-Hole Tension 1 Properties (OHT1) ...................................... 70 3.16 “10/80/10” Open-Hole Tension 2 Properties (OHT2) ...................................... 70 3.17 “50/40/10” Open-Hole Tension 3 Properties (OHT3) ...................................... 71 3.18 “25/50/25” Filled-Hole Tension 1 Properties (FHT1) ....................................... 71 3.19 “10/80/10” Filled-Hole Tension 2 Properties (FHT2) ....................................... 72 3.20 “50/40/10” Filled-Hole Tension 3 Properties (FHT3) ....................................... 72 3.21 “25/50/25” Open-Hole Compression 1 Properties (OHC1) .............................. 73 3.22 “10/80/10” Open-Hole Compression 2 Properties (OHC2) .............................. 73 3.23 “50/40/10” Open-Hole Compression 3 Properties (OHC3) .............................. 74 3.24 “25/50/25” Filled-Hole Compression 1 Properties (FHC1) .............................. 74 3.25 “10/80/10” Filled-Hole Compression 2 Properties (FHC2) .............................. 75 3.26 “50/40/10” Filled-Hole Compression 3 Properties (FHC3) .............................. 75 3.27 “25/50/25” Single-Shear Bearing Strength1 Properties (SSB1) ...................... 76 3.28 “10/80/10” Single-Shear Bearing Strength 2 Properties (SSB2) ..................... 78 3.29 “50/40/10” Single-Shear Bearing 3 Properties (SSB3) .................................... 79 3.30 Compression After Impact 1 Properties (CAI1) ............................................... 80 3.31 Interlaminar Tension Properties (ILT) ............................................................. 81

4. Raw Data ................................................................................................................. 82 4.1 Longitudinal Tension Properties (LT) .............................................................. 82 4.2 Transverse Tension Properties (TT) ............................................................... 90 4.3 Longitudinal Compression Properties (LC) ..................................................... 98 4.4 Transverse Compression Properties (TC)..................................................... 110 4.5 In-Plane Shear Properties (IPS) .................................................................... 122


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4.6 “25/50/25” Unnotched Tension 1 Properties (UNT1) ..................................... 134 4.7 “10/80/10” Unnotched Tension 2 Properties (UNT2) ..................................... 142 4.8 “50/40/10” Unnotched Tension 3 Properties (UNT3) ..................................... 148 4.9 “33/0/67” Unnotched Compression 0 Properties (UNC0) .............................. 154 4.10 “25/50/25” Unnotched Compression 1 Properties (UNC1) ............................ 166 4.11 “10/80/10” Unnotched Compression 2 Properties (UNC2) ............................ 172 4.12 “50/40/10” Unnotched Compression 3 Properties (UNC3) ............................ 176 4.13 Lamina Short-Beam Strength Properties (SBS) ............................................ 180 4.14 Laminate Short-Beam Strength Properties (SBS1) ....................................... 192 4.15 “25/50/25” Open-Hole Tension 1 Properties (OHT1) .................................... 196 4.16 “10/80/10” Open-Hole Tension 2 Properties (OHT2) .................................... 204 4.17 “50/40/10” Open-Hole Tension 3 Properties (OHT3) .................................... 210 4.18 “25/50/25” Filled-Hole Tension 1 Properties (FHT1) ..................................... 216 4.19 “10/80/10” Filled-Hole Tension 2 Properties (FHT2) ..................................... 224 4.20 “50/40/10” Filled-Hole Tension 3 Properties (FHT3) ..................................... 230 4.21 “25/50/25” Open-Hole Compression 1 Properties (OHC1) ............................ 236 4.22 “10/80/10” Open-Hole Compression 2 Properties (OHC2) ............................ 242 4.23 “50/40/10” Open-Hole Compression 3 Properties (OHC3) ............................ 246 4.24 “25/50/25” Filled-Hole Compression 1 Properties (FHC1) ............................ 250 4.25 “10/80/10” Filled-Hole Compression 2 Properties (FHC2) ............................ 256 4.26 “50/40/10” Filled-Hole Compression 3 Properties (FHC3) ............................ 260 4.27 “25/50/25” Single-Shear Bearing 1 Properties (SSB1) .................................. 264 4.28 “10/80/10” Single-Shear Bearing 2 Properties (SSB2) .................................. 272 4.29 “50/40/10” Single-Shear Bearing 3 Properties (SSB3) .................................. 276 4.30 Compression After Impact 1 Properties (CAI1) ............................................. 282 4.31 Interlaminar Tension Properties (ILT) ........................................................... 284

5. Additional Compression After Impact Data ............................................................ 290 6. Full Stress vs. Strain Curves .................................................................................. 291

6.1 Longitudinal Tension - RTD .......................................................................... 291 6.2 Transverse Tension – RTD ........................................................................... 292 6.3 Transverse Compression – RTD ................................................................... 293 6.4 In-Plane Shear – RTD ................................................................................... 294 6.5 “25/50/25” Unnotched Tension 1 – RTD ....................................................... 295 6.6 “10/80/10” Unnotched Tension 2 – RTD ....................................................... 296 6.7 “50/40/10” Unnotched Tension 3 – RTD ....................................................... 297 6.8 “33/0/67” Unnotched Compression 0 – RTD ................................................. 298 6.9 “25/50/25” Unnotched Compression 1 – RTD ............................................... 299 6.10 “10/80/10” Unnotched Compression 2 – RTD ............................................... 300 6.11 “50/40/10” Unnotched Compression 3 – RTD ............................................... 301

7. Fluid Sensitivity Comparison .................................................................................. 302 7.1 Room Temperature Data .............................................................................. 302 7.2 Elevated Temperature Test Data .................................................................. 305 7.3 Load Displacement Curves ........................................................................... 308

8. Moisture Conditioning Charts ................................................................................. 312 8.1 Longitudinal Tension – Thinnest Panel ......................................................... 312 8.2 Short Beam Strength – Thickest Panel ......................................................... 313


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9. DMA Results .......................................................................................................... 314 9.1 DMA Dry Batch A .......................................................................................... 316 9.2 DMA Wet Batch A ......................................................................................... 317

10. Deviations .............................................................................................................. 317


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List of Tables Table 1-1: Lamina Level Test Matrix ............................................................................. 15 Table 1-2: Laminate Level Test Matrix .......................................................................... 16 Table 1-3: Physical Testing Matrix ................................................................................ 17 Table 1-4: Fluid Sensitivity Matrix ................................................................................. 20 Table 2-1: Lamina Summary Data ................................................................................ 22 Table 2-2: Laminate Summary Data.............................................................................. 23

List of Figures

Figure 1-1: Naming Format ........................................................................................... 11 Figure 1-2: Specimen Selection Methodology ............................................................... 13 Figure 1-3: Specimen Traceability Line ......................................................................... 13


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1. Introduction

1.1 Scope

The test methods and results described in this document are intended to provide basic composite properties essential to most methods of analysis and are consistent with CMH-17—Composite Materials Handbook for Polymer Matrix Composites. This report contains material property data of common usefulness to wide range of projects. The lamina and laminate material property data have been generated with NCAMP oversight in accordance with NSP 100 NCAMP Standard Operating Procedures; the test panels and test specimens have been inspected by NCAMP Authorized Inspection Representatives (AIR) and the testing has been witnessed by NCAMP Authorized Engineering Representatives (AER). However, the data may not fulfill all the needs of any specific company's program; specific properties, environments, laminate architecture, and loading situations may require additional testing. The use of NCAMP material and process specifications do not guarantee material or structural performance. Material users should be actively involved in evaluating material performance and quality including, but not limited to, performing regular purchaser quality control tests, performing periodic equivalency/additional testing, participating in material change management activities, conducting statistical process control, and conducting regular supplier audits. The applicability of NCAMP material property data, material allowables, and specifications must be evaluated on case-by-case basis by aircraft companies and certifying agencies. NCAMP assumes no liability whatsoever, expressed or implied, related to the use of the material property data, material allowables, and specifications. This report contains material property data only. Statistical analysis of the data including the calculations of b-basis values is given in a separate report Solvay Cytec Cycom 5320-1 T650 Unitape Gr 145 Qualification Statistical Analysis Report NCP-RP-2013-001 Rev A. The qualification material was procured to NCAMP Material Specification NMS 532/5 Initial Release dated July 6, 2010. The qualification test panels were cured in accordance with NCAMP Process Specification NPS 85321 Rev A dated September 23, 2010 Baseline “C” Cure Cycle. The NCAMP Test Plan NTP 5325Q1 was used for this qualification program. Part fabricators that wish to utilize the material property data, allowables, and specifications may be able to do so by demonstrating the capability to reproduce the original material properties; a process known as equivalency. More information about this equivalency process including the test statistics and its limitations can be found in Section 6 of DOT/FAA/AR-03/19 and Section 8.4.1 of CMH-17. The applicability of equivalency process must be evaluated on program-by-program basis by the applicant and certifying agency. The applicant and certifying agency must agree that the equivalency test plan along with the equivalency process described in Section 6 of DOT/FAA/AR-03/19 and Section 8.4.1 of CMH-17 are adequate for the given program.


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Aircraft companies should not use the data published in this report without specifying NCAMP Material Specification NMS 532/5. NMS 532/5 may have additional requirements that are listed in its prepreg process control document (PCD), fiber specification, fiber PCD, and other raw material specifications and PCDs which impose essential quality controls on the raw materials and raw material manufacturing equipment and processes. Aircraft companies and certifying agencies should assume that the material property data published in this report is not applicable when the material is not procured to NMS 532/5. NMS 532/5 is a free, publicly available, non-proprietary aerospace industry material specification. The data in this report is intended for general distribution to the public, either freely or at a price that does not exceed the cost of reproduction (e.g. printing) and distribution (e.g. postage). 1.2 Symbols

12t major Poisson’s ratio, tension

micro-strain E1

c compressive modulus, longitudinal / warp direction E1

t tensile modulus, longitudinal / warp direction E2

c compressive modulus, transverse / fill direction E2

t tensile modulus, transverse / fill direction F1

cu ultimate compressive strength, longitudinal / warp direction F1

tu ultimate tensile strength, longitudinal / warp direction F2

cu ultimate compressive strength, transverse / fill direction F2

tu ultimate tensile strength, transverse / fill direction SBS short beam strength 12

c major Poisson’s Ratio, compression 21

c minor Poisson’s Ratio, compression F12

s5% strain in-plane shear strength at 5% strain F12

smax in-plane shear peak strength before 5% strain F12

s0.2% in-plane shear strength at 0.2% offset G12

s in-plane shear modulus Superscripts c compression cu compression ultimate s shear su shear ultimate t tension tu tension ultimate


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Subscripts 1 axis; longitudinal / warp direction (parallel to warp direction

of reinforcement) 2 axis; transverse / fill direction (parallel to fill direction of

reinforcement) 12 in-plane Acronyms and Definitions ASTM American Society for Testing and Materials B – Basis 95% lower confidence limit on the tenth population percentile CV Coefficient of variation CTD cold temperature dry CPT cured ply thickness ETD elevated temperature dry ETW elevated temperature wet Gr/Ep graphite/epoxy norm normalized RTD room temperature dry SACMA Suppliers of Advanced Composite Materials Association SRM SACMA Recommended Method Tply thickness divided by the number of plies provides the

thickness average per specimen wet specimen with an “equilibrium” moisture content T, RH temperature, relative humidity


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1.3 NIAR–Specimen Naming Format

Figure 1-1: Naming Format


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1.4 References

ASTM Standards

All testing was in accordance with nationally recognized standards, methods and procedures. Specific mechanical property test methods applicable to the test program in this document include:

ASTM D2344/D2344M-00(2006) – Standard Test Method for Short-Beam Strength of Polymer Matrix Composite Materials and Their Laminates

ASTM D3039/D3039M-08 – Standard Test Method for Tensile Properties of Polymer Matrix Composite Materials

ASTM D3518/D3518M-94(2007) – Standard Test Method for In-Plane Shear Response of Polymer Matrix Composite Materials by Tensile Test of a ± 45º Laminate In-Plane Shear Strength and Modulus

ASTM D5766/D5766M-07 – Standard Test Method for Open Hole Tensile Strength of Polymer Matrix Composite Laminates

ASTM D5961/D5961M-08 – Standard Test Method for Bearing Response of Polymer Matrix Composite Laminates

ASTM D6415-06ae1 – Standard Test Method for Measuring the Curved Beam Strength of a Fiber-Reinforced Polymer-Matrix Composite

ASTM D6484/D6484M-04 – Standard Test Method for Open-Hole Compressive Strength of Polymer Matrix Composite Laminates

ASTM D6641/D6641M-01e1 – Standard Test Method for Determining the Compressive Properties of Polymer Matrix Composite Laminates Using a Combined Loading Compression (CLC) Test Fixture

ASTM D6742/D6742M-07 – Standard Practice for Filled-Hole Tension and Compression Testing of Polymer Matrix Composite Laminates

ASTM D7028-07e1 – Standard Test Method for Glass Transition Temperature (DMA Tg) of Polymer Matrix Composites by Dynamic Mechanical Analysis (DMA)

ASTM D7136/D7136M-07 – Standard Test Method for Measuring the Damage Resistance of a Fiber-Reinforced Polymer Matrix Composite to a Drop-Weight Impact Event

ASTM D7137/D7137M-07 – Standard Test Method for Compressive Residual Strength Properties of Damaged Polymer Matrix Composite Plates


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1.5 Methodology

1.5.1 Process Definition

For each combination of test, batch and condition, the specimens were selected from minimum two separate panels cured separately as shown in Figure 1-2 unless otherwise specified.

PER ENVIRONMENTAL CONDITION AND TEST METHOD

MaterialBatch

PanelManufacturing& IndependentCure Process

Number ofSpecimens

Required perTest Method &Environment

BATCH 2

PANEL 4

3 spec.

PANEL 3

3 spec.

BATCH 3

PANEL 6

3 spec.

PANEL 5

3 spec.

BATCH 1

PANEL 2

3 spec.

PANEL 1

3 spec.

18 SPECIMENS TOTAL

Figure 1-2: Specimen Selection Methodology

All panels were fabricated in accordance with NCAMP process specification 85321 “C” Cure Cycle. In order to facilitate individual specimen trace ability, individual specimen numbering and/or skewed lines were written or drawn across each sub-panel as shown in Figure 1-3.

Figure 1-3: Specimen Traceability Line


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1.5.2 Specimen & Testing Details

1.5.2.1 Tabbing Longitudinal Tension coupons were tabbed with Solvay Cytec FM 300-2M and ±45° Unbeveled Glass tabstock.

1.5.2.2 Specimen Dimensions & Test Configuration For filled-hole and bearing tests, the hole diameter was 0.25 in -0.000 +0.003 in. For filled-hole tension tests, the fasteners were installed to 85±5 in-lb. For filled-hole compression and bearing tests, the fasteners were installed to 30±5 in-lb. Fasteners were installed after moisture conditioning. Unless otherwise specified, a tolerance of ±5°F applied to all temperature conditions specified in this document. For filled-hole and bearing tests, the hole diameter was 0.25 in -0.000 +0.003 in. The following fasteners were used:

1) NASM 21297-04003 bolts with MS 21084 nuts and MS 21206 washers for FHT and FHC1

2) NASM 14181-04004 bolts with MS 14182 nuts and MS14183 washers for FHC2 and FHC3

3) NASM 21297-04016 bolts with MS 21084 nuts and MS 21206 washers for SSB


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1.5.3 Test Matrix

The tables below show the lay-ups and test matrices used for lamina and laminate level testing.

Table 1-1: Lamina Level Test Matrix Note 1: Back-to-back strain gages are needed on the first two specimens of RTD environment. If no buckling is observed, the remaining modulus specimens will require a strain gage on one side of the specimens only. An appropriate extensometer may be used in place of the strain gage. Note 2: Gripped (tab) length is 1.5±0.5” on each end of the 10” long specimen. Once the samples have reached the 5% strain level, the actuator/crosshead displacement rate can be increased by four times the initial rate. Continue testing at the higher strain rate until ultimate failure is observed. Note 3: If strain gage is used for modulus measurement, a separate un-gaged specimen must be used for strength measurement; because the strain gage and its protective coating may prevent moisture absorption in the gage area. Note 4: At least two specimens must be gaged to obtain full stress-strain curve to failure. An appropriate extensometer may be used in place of the strain gage for the remaining specimens.

Note 5: Derive the 0° lamina compressive strength 0F cu

plies as follows

1

0 0 /900 /90

F Fcu cuplies

E

E

Where:

0Fcuplies = 0° ply Strength

0 /90Fcu = 0°/90° or 90°/0° cross-ply laminate strength

1E = 0° Modulus

0 /90E = 0°/90° or 90°/0° cross-ply laminate modulus


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Table 1-2 below summarizes the laminate level tests carried out. The layup angles 0º, 45º, -45º, and 90º refer to the orientation of the warp/longitudinal fiber direction. The laminate stacking sequences in this program are not specific to any design. Therefore, careful consideration should be given to the validity of properties derived from this program based on the design specific laminates in a structure to be certified. Table 1-2 also emphasizes those properties and test condition combinations believed to constitute the worst case, which in general is cold dry for tension and hot wet for compression and other matrix dominated properties.

Table 1-2: Laminate Level Test Matrix


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Note 1: Open-hole configuration: 0.25” hole diameter, 1.5 inch width. Note 2: Filled-hole test configuration: 0.25” diameter, see section 1.5.2.2 for fastener callout, 1.5” width. Note 3: Single shear bearing test configuration: 0.25: hole diameter, 1.5” width, see section 1.5.2.2 for

fastener callout, e/D=3, ASTM D5961-08 Procedure C Note 4: Back-to-back strain gages needed on the first two specimens of each environment. If no buckling

is observed, the remaining modulus specimens will require strain gage on one side of the specimens only. Appropriate extensometer may be used in place of the strain gage.

Note 5: Loading direction is generally along the 0-degree direction Note 6: If strain gage is used for modulus measurement, a separate un-gaged specimen must be used

for strength measurement, because the strain gage and its protective coating may prevent moisture absorption in the gage area.

Note 7: At least two specimens must be gaged to obtain full stress-strain curve to failure. An appropriate extensometer may be used in place of the strain gage for the remaining specimens.

1.5.4 Cured Laminate Physical Testing

The properties in Table 1-3: Physical Testing MatrixTable 1-3 were determined for each panel used for test coupons with the exception of Tg by DMA which were conducted on one laminate per batch from each oven cure conducted where that batch is present. The tests were performed by the National Institute for Aviation Research (NIAR) Composites Laboratory under the supervision of NCAMP.

Table 1-3: Physical Testing Matrix

Note 1: Where the applicable standard allows variations in specimen form or test method, the specific

parameters to be used will be specified in the test work instructions and reported in the final test report.

Note 2: Method II, except for laminates of materials where actual fiber weight is not accurately known prior to impregnation, as in the case for unidirectional materials. For these materials, in order to verify Method II is accurate, a minimum of 12 samples per batch shall be tested by Method I, Procedure B.

Note 3: Five MHz is preferred for solid laminates. Panels with anomaly should be segregated. Microscopy images may be taken from questionable areas. NCAMP must be involved in the review of all C-scans.

Note 4: Minimum total of 24 dry and 24 wet for each material system. Note 5: To be performed by Solvay Cytec Engineered Materials, Greenville, TX


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1.5.5 Environmental Conditioning

The following tests were performed by the NIAR Composites Laboratory under the supervision of NCAMP.

CTD = -65±5°F, dry RTD = 70±10°F, dry ETD1 = 180±5°F, dry ETW1 = 180±5°F, wet ETD2 = 250±5°F, dry ETW2 = 250±5°F**, wet

** If the wet glass transition temperature as determined in Table 1-3 is not 300°F or higher, the ETW2 test temperature will be reduced to 50°F below the measured wet glass transition temperature. Within each test method and test environment, the failure mode was evaluated immediately after each test by an NCAMP staff engineer or NCAMP AER. All tested specimens were digitally photographed after each test in order to pictorially document failure modes. Representative photos are included in the CD accompanying this report. For dry testing, specimens were dried at 250°F±5°F for at least 24 hours. After drying, specimens were kept in a desiccator until mechanical testing. Alternatively, the specimens may have been left ambient laboratory condition for a maximum of 14 days until mechanical testing (no drying was required if specimens were tested within 14 days from the date they were cured). Ambient laboratory condition is defined as 70°F±10°F. Since moisture absorption and desorption rate for epoxy is very slow at ambient temperature, there was no requirement to maintain relative humidity levels. For wet conditioning, specimens were dried at 250°F±5°F for 24 hours minimum before being conditioned to equilibrium at 160°F±5°F and 85% ± 5%. Effective moisture equilibrium is achieved when the average moisture content of the traveler specimen changes by less than 0.02% for two consecutive determinations which are 7 ±0.5 days apart and may be expressed by:

0002.01

b

ii

W

WW

Where: Wi = weight at current time Wi – 1 = weight at previous time Wb = baseline weight prior to conditioning

When representative specimens could not be measured to determine the moisture content (due to size, fastener and tab effects), traveler coupons of at least 1” by 1” by specimen thickness and weighing at least 15 grams were used to establish weight gain measurements. If the specimens or traveler coupons pass the criteria for two consecutive readings which are 7 ±0.5 days apart, the specimens were kept in the environmental chamber for up to an additional 60 days. Alternatively, the specimens


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may have been removed from the environmental chamber and placed in a sealed plastic bag along with a moist cotton towel for a maximum of 14 days until mechanical testing. Strain-gaged specimens were removed from the controlled environment for a maximum of 2 hours for application of gages in ambient laboratory conditions.

1.5.6 Non-ambient Testing

The chamber was of adequate size so that all test fixtures and load frame grips were contained within the chamber. For elevated temperature testing, the temperature chamber, test fixture, and grips were preheated to the specified temperature. Each specimen was heated to the required test temperature as verified by a thermocouple in direct contact with and taped to the specimen gage section. The heat-up time of the specimen did not exceed 5 minutes, unless otherwise specified in individual test summary sheets. The test was started

1 0 5

minutes after the specimen reached the test temperature. During the test, the temperature, as measured on the specimen, was within 5°F of the required test temperature. For subzero temperature testing, each specimen was cooled to the required test temperature as verified by a thermocouple in direct contact with and taped to the

specimen gage section. The test started 1 0 5

minutes after the specimen reached the test temperature. During the test, the temperature, as measured on the specimen, was within 5°F of the required test temperature. For wet specimens, the moisture loss was determined by subjecting representative specimens to the same amount of time required to heat-up and fail the specimens. For filled-hole or bearing specimens, fasteners were removed prior to conducting moisture loss measurements. For tabbed specimens, representative coupons without tabs and having the same number of plies were used to conduct the moisture loss measurements. A minimum of one specimen or representative coupon was used to measure the moisture loss for every combination of test temperature and stacking sequence. 1.5.7 Fluid Sensitivity Screening

Table 1-4 lists the requirements for fluid sensitivity screening, which requires ASTM D2344 Short Beam Strength testing on [0°]20 lamina level specimens dried at 250°F±5°F for 24 hours minimum before being subjected to the conditions indicated, five replicates per fluid and one cure cycle. Specimens were cleaned with a dry towel prior to the tests. In addition to short beam strength, load versus displacement curves were plotted to aid in the identification of matrix/resin softening. Since load versus displacement curves are influenced by test machine and fixture compliance, all the tests


of 317

were performed with the identical machine and fixture, through a single setup. Experience suggests that for the vast majority of epoxy resins, water is the fluid with the most deleterious effect on properties. Should screening tests for fluid sensitivity indicate this to be the case, further testing of this type might be unnecessary since exposure to water moisture to equilibrium level is an inherent part of the multi batch allowables test program. However, users must evaluate the applicability of the exposure conditions and time on case-by-case basis. For example, the exposure condition for jet fuel may not fully represent the condition of integral fuel tanks.

Table 1-4: Fluid Sensitivity Matrix


of 317

1.5.8 Normalization Procedures

Most lamina level tension and compression strength and modulus properties, and all laminate level properties were normalized according to nominal cured ply thickness. Lamina level properties that were not normalized include 90º tensile strength and modulus (unidirectional only), 90º compressive strength and modulus (unidirectional only), in-plane shear strength and modulus, Poisson’s ratio, SBS, and ILT. After normalizing, data scatter reduced or remained the same. If data scatter increased significantly after normalizing, the reason was investigated. Wherever properties are normalized, both measured and normalized data were reported. For unidirectional materials the fiber areal weight cannot be measured in advance of impregnation, hence Method I of ASTM D3171, utilizing acid digestion, will be used to verify the CPT method in accordance with note (2) of Table 1-3. Method I Fiber Volume (%vol) is 58.67 and Method 2 Fiber Volume (%vol) is 59.20. By comparing Fiber Volume values obtained from Method I and Method II, the values are deemed close enough therefore the FAW is close to the nominal of ~145 gsm. Based on the FAW data from Solvay Cytec (Avg of 144 gsm) and the obtained Method 1 Physical Test data (with an avg void content ~ 0.24%), it is appropriate to use the CPT Method for normalization. The average cured ply thickness of 0.0055 inch has been used as the nominal cured ply thickness (CPT) for normalization purpose. The following normalization formula was used:

Normalized Value = Measured Value x Measured CPT / Nominal CPT 1.5.9 Inspection Verification

The 3-batch qualification panels have been fabricated according to the requirements of the test plan and conformed by an NCAMP AIR. The test specimens and test setup have also been conformed by an NCAMP AIR. Testing was witnessed by NCAMP. Witnessing was delegated to an AER. Mechanical testing was carried out at the National Institute for Aviation Research, Wichita State University. The conformity documentation, with required approval signatures, is included in the CD provided with this report. 1.5.10 Material Pedigree Information

The PMC Data Collection Template includes the material pedigree information required, such as material and batch information, as well as panel fabrication record, environmental conditioning, test equipment, and test procedures. This template in Microsoft Excel file format is included on the CD provided with this report.


of 317

2. Test Results

2.1 Lamina Level Test Summary

Prepreg Material: Cytec 5320-1 T650 Unitape Gr 145 RC 33%

Material Specification: NMS 532/5

Process Specification: NPS 85321 Baseline Cure Cycle CFiber: T650 Unitape Resin: Cycom 5320-1

Tg(dry): 389.13 °F Tg(wet): 321.79 °F Tg METHOD: ASTM D7028

Date of fiber manufacture Apr 2010, Apr-May 2011 Date of testing Mar-Oct 2012Date of resin manufacture Aug 2011 Date of data submittal Feb 2013Date of prepreg manufacture Aug 2011Date of composite manufacture Sept-Dec 2011

Normalized Measured Normalized Measured Normalized Measured Normalized Measured Normalized Measured Normalized Measured

F1tu [ksi] 293.615 292.317 299.093 299.004 272.989 276.017 274.431 272.069

E1t [Msi] 20.214 20.128 20.082 20.077 20.030 20.263 20.084 19.892

0.325 0.326 0.334 0.337

F2tu [ksi] --- 10.975 --- 10.096 --- 8.432 --- 4.730

E2t [Msi] --- 1.485 --- 1.331 --- 1.213 --- 0.840

F1cu [ksi] 251.251 251.646 237.098 237.875 228.986 227.566 197.980 197.413 218.848 218.226 179.138 177.128

from UNC0*

E1c [Msi] 17.256 17.308 18.301 18.356 18.454 18.407 18.534 18.550 18.271 18.220 18.252 18.216

F2cu [ksi] --- 51.397 --- 39.751 --- 31.141 --- 25.231 --- 26.248 --- 19.364

E2c [Msi] --- 1.531 --- 1.427 --- 1.301 --- 1.292 --- 1.244 --- 1.094

UNC0 Strength [ksi] 97.657 98.354 91.892 92.510 86.522 86.381 75.570 76.027 83.682 83.368 67.275 67.481

UNC0 Modulus [Msi] 6.707 6.765 7.093 7.139 6.973 6.987 7.074 7.144 6.987 6.961 6.855 6.940

F12s0.2% [ksi] --- 11.269 --- 8.121 --- 5.151 --- 3.060

F12smax [ksi] --- 17.198 --- --- --- --- --- ---

F12s5%strain [ksi] --- --- --- 13.501 --- 8.165 --- 5.139

G12s [Msi] --- 0.838 --- 0.718 --- 0.547 --- 0.325

SBS [ksi] --- 18.126 --- 15.639 --- 11.730 --- 10.250 --- 9.665 --- 7.722

Cytec 5320-1 T650 Unitape Gr 145 RC 33%

Lamina Properties Summary

LAMINA MECHANICAL PROPERTY SUMMARYData reported as: Normalized & Measured

(Normalized by CPT=0.0055 inch)

CTD Mean RTD Mean ETD1 Mean ETW1 Mean ETD2 Mean ETW2 Mean

Table 2-1: Lamina Summary Data


of 317

2.2 Laminate Level Test Summary

Prepreg Material: Cytec 5320-1 T650 Unitape Gr 145 RC 33%Material Specification: NMS 532/5Process Specification: NPS 85321 Baseline Cure Cycle CFiber: T650 Unitape Resin: Cycom 5320-1

Tg(dry): 389.13 °F Tg(wet): 321.79 °F Tg METHOD: ASTM D7028

Date of fiber manufacture Apr 2010, Apr-May 2011 Date of testing Mar-Oct 2012Date of resin manufacture Aug 2011 Date of data submittal Feb 2013Date of prepreg manufacture Aug 2011Date of composite manufacture Sept-Dec 2011

Layup:Test Condition Normalized Measured Normalized Measured Normalized Measured

CTD 47.105 47.046 44.056 43.732 65.202 64.585RTD 49.601 49.605 42.535 42.191 70.597 69.906

ETW1 52.842 52.375 --- --- --- ---ETW2 53.675 53.427 35.238 34.909 86.585 85.508RTD 50.894 50.684 44.484 44.400 66.016 65.929

ETW1 44.630 44.446 --- --- --- ---ETW2 39.199 39.002 32.389 32.252 52.759 52.603CTD 92.513 92.199 71.302 70.795 144.363 143.639RTD 97.622 97.737 67.633 67.581 153.345 152.653

ETW1 105.189 105.614 --- --- --- ---ETW2 103.351 102.659 50.130 49.782 164.899 163.352CTD 7.709 7.683 5.124 5.089 11.805 11.750RTD 7.580 7.590 4.917 4.914 11.698 11.641

ETW1 7.209 7.238 --- --- --- ---ETW2 6.963 6.916 4.173 4.144 11.574 11.489RTD 96.628 97.952 72.330 73.618 129.217 130.454

ETW1 81.676 81.965 --- --- --- ---ETW2 68.635 68.666 43.957 43.965 86.522 86.791RTD 7.189 7.301 4.743 4.842 10.913 11.041

ETW1 7.172 7.171 --- --- --- ---ETW2 6.752 6.764 3.932 3.927 10.463 10.509CTD 56.416 56.125 51.295 51.297 70.552 70.159RTD 57.962 57.744 49.558 49.549 77.031 76.861

ETW1 60.602 60.648 --- --- --- ---ETW2 60.048 59.695 39.898 39.805 83.001 82.528RTD 81.560 81.291 61.954 61.727 94.140 93.816

ETW1 67.154 66.868 --- --- --- ---ETW2 55.757 55.575 41.262 41.030 71.163 70.894RTD --- 13.710

ETW2 --- 7.356RTD 135.155 138.099 --- --- 129.575 130.664

ETW1 114.633 115.963 --- ---ETW2 101.299 101.461 --- --- 100.496 100.224RTD 136.627 139.642 134.738 135.741 137.336 138.310

ETW1 113.335 114.664ETW2 102.565 102.719 101.082 100.954 102.704 102.392RTD 151.576 154.903 161.861 163.020 145.805 146.834

ETW1 130.335 131.854ETW2 113.840 114.010 120.367 120.198 120.521 120.150CTD --- 238.501RTD --- 251.215

ETW2 --- 153.369CTD --- 6.831RTD --- 7.399

ETW2 --- 4.719CAI Strength [ksi] RTD 24.280 24.270* lay up is 100/0/0

UNC Modulus [Msi]


Laminate Properties Summary

LAMINATE MECHANICAL PROPERTY SUMMARYData reported as: Normalized & Measured

(Normalized by CPT=0.0055 inch)

25/50/25 10/80/10 50/40/10

OHT Strength [ksi]

OHC Strength [ksi]

UNT Strength [ksi]

UNT Modulus [Msi]

UNC Strength [ksi]

ILT [ksi]*

SSB 2% Offset Strength [ksi]

FHT Strength [ksi]

FHC Strength [ksi]

SBS1 Strength [ksi]

SSB Initial Peak Bearing Strength [ksi]

SSB Ultimate Bearing Strength [ksi]

CBS [lb]*

Table 2-2: Laminate Summary Data


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2.3 Individual Test Summaries

2.3.1 Longitudinal Tension Properties (LT)

Material:

Resin content: 30.66 % wt Comp. density: 1.574 g/cc

Fiber volume: 61.88 % vol

Ply count: 8

Test method: ASTM D 3039-08

Normalized by: 0.0055 in. CPT

Normalized Measured Normalized Measured Normalized Measured Normalized MeasuredMean 293.615 292.317 299.093 299.004 272.989 276.017 274.431 272.069Minimum 260.542 266.291 272.717 269.754 241.145 248.616 236.839 234.704Maximum 323.949 311.839 324.928 320.612 303.649 305.972 312.116 304.278C.V.(%) 4.958 4.318 5.290 5.244 8.835 8.285 8.535 8.244

No. Specimens

No. Prepreg Lots

Mean 20.214 20.128 20.082 20.077 20.030 20.263 20.084 19.892Minimum 19.248 19.469 18.685 19.536 18.806 19.670 19.202 19.354Maximum 20.884 20.620 20.860 20.695 20.693 20.891 20.703 20.546C.V.(%) 2.175 1.619 2.195 1.313 3.065 2.291 2.056 1.428

No. Specimens

No. Prepreg Lots

Mean 0.325 0.326 0.334 0.337

No. Specimens

No. Prepreg Lots

22

3

Tension, 1-axis Cytec 5320-1 T650 Unitape Gr 145 RC 33%

[0]8

23

3

22

31

7

1

ETW2

250

Equilbrium

160 F,85%

CUGJX XXXFCUGJX XXXD

8

1

720

3

20

3

21

3

RTD

70

Dry

CUGJX XXXA

21

3

21

3

21

3

F1tu [ksi]

E1t [Msi]

12


Modulus calculation: 1000 to 3000 microstrain

Test Temperature [°F]

Moisture Conditioning

Equilbrium at T, RH

CTD

-65

Dry

Source code

ETW1

180

Equilbrium

160 F,85%

CUGJX XXXB


of 317

2.3.2 Transverse Tension Properties (TT)

Material:



Ply count: 16


Normalized by: NA

Normalized Measured Normalized Measured Normalized Measured Normalized MeasuredMean 10.975 10.096 8.432 4.730Minimum 7.610 8.171 7.083 3.546Maximum 13.142 11.459 8.844 5.960C.V.(%) 13.251 8.045 7.278 12.327

No. Specimens

No. Prepreg Lots

Mean 1.485 1.331 1.213 0.840Minimum 1.415 1.291 1.178 0.804Maximum 1.577 1.403 1.241 0.874C.V.(%) 3.218 1.859 1.796 2.367

No. Specimens

No. Prepreg Lots





Equilbrium at T, RH

RTD

70

Dry

Tension, 2-axis Cytec 5320-1 T650 Unitape Gr 145 RC 33%

[90]16

ETW2

250

Equilbrium

160 F,85%

ETW1

180

F2tu [ksi]

E2t [Msi]

CTD

-65

Dry

CUGUX XXXB

24

Source code

3

21

3

CUGUX XXXA

7

1

21

3

21

3

24

3

Equilbrium

160 F,85%

24

3

CUGUX XXXF

7

1

CUGUX XXXD


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2.3.3 Longitudinal Compression Properties (LC)

Material:



Ply count: 20



Normalized Measured Normalized Measured Normalized Measured Normalized Measured Normalized Measured Normalized MeasuredMean 17.256 17.308 18.301 18.356 18.454 18.407 18.534 18.550 18.271 18.220 18.252 18.216Minimum 15.232 15.000 17.791 17.868 18.304 18.247 17.895 18.094 18.119 18.058 17.198 17.093Maximum 21.898 22.407 18.741 19.023 18.646 18.615 19.312 19.573 18.409 18.303 19.068 19.083C.V.(%) 10.064 10.447 1.328 1.633 0.671 0.707 2.284 2.585 0.611 0.457 2.488 2.863

No. Specimens

No. Prepreg Lots

Compression, 1-axisCytec 5320-1 T650 Unitape Gr 145 RC 33%

[0]20

7

1

ETW2

250

Equilbrium

160 F,85%

CUGLX XXXF

21

3

ETD2

250

Dry

CUGLX XXXE

7

1

ETW1

180

Equilbrium

160 F,85%

CUGLX XXXD

7

1

CUGLX XXXA

21

3

ETD1

180

Dry

CUGLX XXXC

E1c [Msi]

CTD

-65

Dry

CUGLX XXXB

21

3

Source code





Equilbrium at T, RH

RTD

70

Dry


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2.3.4 Transverse Compression Properties (TC)

Material:



Ply count: 20


Normalized by: NA

Normalized Measured Normalized Measured Normalized Measured Normalized Measured Normalized Measured Normalized MeasuredMean 51.397 39.751 31.141 25.231 26.248 19.364Minimum 46.520 35.507 28.982 24.457 24.300 18.232Maximum 53.834 41.579 33.144 26.262 27.387 20.350C.V.(%) 4.200 3.931 4.282 2.715 3.841 2.913

No. Specimens

No. Prepreg Lots

Mean 1.531 1.427 1.301 1.292 1.244 1.094Minimum 1.485 1.353 1.274 1.249 1.221 0.999Maximum 1.583 1.646 1.353 1.373 1.276 1.194C.V.(%) 1.875 4.673 1.977 3.097 1.435 5.618

No. Specimens

No. Prepreg Lots 3

Compression, 2-axisCytec 5320-1 T650 Unitape Gr 145 RC 33%

[90]20

ETW2

250

Equilbrium

160 F,85%

ETD2

250

Dry

CUGZX XXXF

7

CUGZX XXXE

21

3

7 21

1

7

1

7

1

1

ETW1

180

Equilbrium

160 F,85%

CUGZX XXXD

7

1

7

1

23

3

21

3

CUGZX XXXA

ETD1

180

Dry

CUGZX XXXC

F2cu [ksi]

E2c [Msi]

CTD

-65

Dry

CUGZX XXXB

21

Source code

3

21

3





Equilbrium at T, RH

RTD

70

Dry


of 317

2.3.5 In-Plane Shear Properties (IPS)

Material:



Ply count: 16


Normalized by: NA

Normalized Measured Normalized Measured Normalized Measured Normalized MeasuredMean 11.269 8.121 5.151 3.060Minimum 10.639 7.820 5.023 2.668Maximum 12.321 8.430 5.283 3.430C.V.(%) 3.999 1.468 1.608 5.451

No. Specimens

No. Prepreg Lots

Mean 17.198Minimum 16.245Maximum 18.252C.V.(%) 3.004

No. Specimens

No. Prepreg Lots

Mean 13.501 8.165 5.139Minimum 13.055 7.935 4.695Maximum 13.697 8.297 5.438C.V.(%) 1.278 1.568 3.874

No. Specimens

No. Prepreg Lots


No. Specimens

No. Prepreg Lots

21

23

3

In-Plane ShearCytec 5320-1 T650 Unitape Gr 145 RC 33%

[45/-45]4S

23

3

20

31

7

1

ETW2

250

Equilbrium

160 F,85%

CUGNX XXXFCUGNX XXXD

7

1

621

3

21

3

21

3

21

3

21

3

F12s0.2% [ksi]

F12s5%strain [ksi]

G12s [Msi]

F12smax [ksi]

3





Equilbrium at T, RH

CTD

-65

Dry

RTD

70

Dry

Source code

ETW1

180

Equilbrium

160 F,85%

CUGNX XXXB CUGNX XXXA


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2.3.6 “25/50/25” Unnotched Tension 1 Properties (UNT1)

Material:



Ply count: 16




No. Specimens

No. Prepreg Lots

Mean 7.709 7.683 7.580 7.590 7.209 7.238 6.963 6.916Minimum 7.416 7.441 7.366 7.343 6.921 6.942 6.696 6.615Maximum 7.874 7.887 7.939 7.977 7.534 7.627 7.483 7.458C.V.(%) 1.368 1.371 1.849 2.076 3.445 3.600 3.287 3.108

No. Specimens

No. Prepreg Lots

21

3

Equilbrium

160 F,85%

21

3

CUGAX XXXF

7

1

CUGAX XXXDCUGAX XXXA

7

1

21

3

21

3

UNT1 Strength [ksi]

UNT1 Modulus [Msi]

CTD

-65

Dry

CUGAX XXXB

21

Source code

3

21

3





Equilbrium at T, RH

RTD

70

Dry

Unnotched Tension 1Cytec 5320-1 T650 Unitape Gr 145 RC 33%

[45/0/-45/90]2S

ETW2

250

Equilbrium

160 F,85%

ETW1

180


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Material:



Ply count: 20



Normalized Measured Normalized Measured Normalized MeasuredMean 71.302 70.795 67.633 67.581 50.130 49.782Minimum 67.044 66.653 64.502 63.838 47.580 47.045Maximum 76.326 75.468 70.643 70.976 51.761 52.084C.V.(%) 3.711 3.217 2.800 2.884 2.119 2.456

No. Specimens

No. Prepreg Lots


No. Specimens

No. Prepreg Lots 3

21

3

21

3

21

3

21

CUGBX XXXA

ETW2

250

Equilbrium

160 F,85%

CUGBX XXXF

UNT2 Strength [ksi]

UNT2 Modulus [Msi]

CTD

-65

Dry

CUGBX XXXB

21

Source code

3

21

3





Equilbrium at T, RH


[45/-45/0/45/-45/90/45/-45/45/-45]S

RTD

70

Dry


of 317


Material:



Ply count: 20




No. Specimens

No. Prepreg Lots


No. Specimens

No. Prepreg Lots





Equilbrium at T, RH


[0/45/0/90/0/-45/0/45/0/-45]S

RTD

70

Dry

UNT3 Strength [ksi]

UNT3 Modulus [Msi]

CTD

-65

Dry

CUGCX XXXB

21

Source code

3

21

3

CUGCX XXXA

ETW2

250

Equilbrium

160 F,85%

CUGCX XXXF

3

21

3

22

3

21

3

23


of 317

2.3.9 “33/0/67” Unnotched Compression 0 Properties (UNC0)

Material:



Ply count: 21



Normalized Measured Normalized Measured Normalized Measured Normalized Measured Normalized Measured Normalized MeasuredMean 97.657 98.354 91.892 92.510 86.522 86.381 75.570 76.027 83.682 83.368 67.275 67.481Minimum 82.923 84.042 81.603 82.226 80.661 80.801 71.961 72.495 78.209 78.574 58.125 58.062Maximum 113.079 113.808 101.879 105.098 90.716 90.111 77.904 78.453 88.605 88.500 74.912 75.377C.V.(%) 7.483 7.648 5.573 5.846 3.987 3.810 2.614 2.829 4.603 4.497 5.581 5.765

No. Specimens

No. Prepreg Lots

Mean 6.707 6.765 7.093 7.139 6.973 6.987 7.074 7.144 6.987 6.961 6.855 6.940Minimum 5.989 5.968 6.744 6.843 6.856 6.782 6.742 6.909 6.687 6.668 6.442 6.529Maximum 7.284 7.304 7.562 7.502 7.186 7.299 7.467 7.478 7.104 7.054 7.468 7.525C.V.(%) 5.914 6.228 2.706 2.112 1.789 2.751 3.701 3.068 2.022 1.913 3.610 4.069

No. Specimens

No. Prepreg Lots





Equilbrium at T, RH

RTD

70

Dry

UNC0 Strength [ksi]

UNC0 Modulus [Msi]

CTD

-65

Dry

CUGRX XXXB

21

Source code

3

21

3

CUGRX XXXA

ETD1

180

Dry

CUGRX XXXC

7

1

21

3

21

3

11

1

ETW1

180

Equilbrium

160 F,85%

CUGRX XXXD

1

7

1

7

1

1 3

7 21

3

Unnotched Compression 0/90Cytec 5320-1 T650 Unitape Gr 145 RC 33%

[90/0/90]7

ETW2

250

Equilbrium

160 F,85%

ETD2

250

Dry

CUGRX XXXF

7

CUGRX XXXE

21


of 317


Material:



Ply count: 24




No. Specimens

No. Prepreg Lots


No. Specimens

No. Prepreg Lots





Equilbrium at T, RH

Unnotched Compression 1Cytec 5320-1 T650 Unitape Gr 145 RC 33%

[45/0/-45/90]3S

ETW1

180

Equilbrium

160 F,85%

UNC1 Strength [ksi]

UNC1 Modulus [Msi]

RTD

70

Dry

CUGWX XXXA

22

Source code

3

21

3

CUGWX XXXD

ETW2

250

Equilbrium

160 F,85%

CUGWX XXXF

3

9

1

7

1

22

3

21


of 317


Material:



Ply count: 20



Normalized Measured Normalized MeasuredMean 72.330 73.618 43.957 43.965Minimum 64.583 68.731 40.233 40.288Maximum 77.006 78.152 48.163 47.853C.V.(%) 5.475 4.543 4.408 4.665

No. Specimens

No. Prepreg Lots


No. Specimens

No. Prepreg Lots

RTD

70

Dry

CUGXX XXXA

20

3



Equilbrium at T, RH

Source code

UNC2 Strength [ksi]

UNC2 Modulus [Msi]

21


[45/-45/0/45/-45/90/45/-45/45/-45]S

3

21

3

ETW2

250

Equilbrium

160 F,85%

CUGXX XXXF



21

3


of 317


Material:



Ply count: 20




No. Specimens

No. Prepreg Lots


No. Specimens

No. Prepreg Lots


[45/0/90/0/-45/0/45/0/-45/0]S

3

21

3

ETW2

250

Equilbrium

160 F,85%

CUGYX XXXF



20

3

21

3



Equilbrium at T, RH

Source code

UNC3 Strength [ksi]

UNC3 Modulus [Msi]

21

RTD

70

Dry

CUGYX XXXA


of 317

2.3.13 Lamina Short-Beam Strength Properties (SBS)

Material:



Ply count: 45


Normalized by: NA

Normalized Measured Normalized Measured Normalized Measured Normalized Measured Normalized Measured Normalized MeasuredMean 18.126 15.639 11.730 10.250 9.665 7.722Minimum 16.003 14.502 11.071 9.862 9.481 7.327Maximum 19.986 16.698 12.103 10.578 9.878 8.202C.V.(%) 4.936 3.720 2.853 2.794 1.574 3.159

No. Specimens

No. Prepreg Lots




Equilbrium at T, RH

RTD

70

Dry

SBS Strength [ksi]

CTD

-65

Dry

CUGQX XXXB

23

3

Source code CUGQX XXXA

21

3

ETD1

180

Dry

CUGQX XXXC

7

1

ETW1

180

Equilbrium

160 F,85%

CUGQX XXXD

7

1

Short-Beam StrengthCytec 5320-1 T650 Unitape Gr 145 RC 33%

[0]45

8

1

ETW2

250

Equilbrium

160 F,85%

CUGQX XXXF

22

3

ETD2

250

Dry

CUGQX XXXE


of 317

2.3.14 Laminate Short-Beam Strength Properties (SBS1)

Material:



Ply count: 32


Normalized by: NA

Normalized Measured Normalized MeasuredMean 13.710 7.356Minimum 11.168 6.943Maximum 14.499 8.102C.V.(%) 6.205 5.199

No. Specimens

No. Prepreg Lots

Laminate Short-Beam StrengthCytec 5320-1 T650 Unitape Gr 145 RC 33%

[45/0/-45/90]4S


ETW2

250Test Temperature [°F]

RTD

70

Dry

21

CUGqX XXXA

21

3


Equilbrium at T, RH

SBS1 Strength [ksi]

3

Source code

Equilbrium

160 F,85%

CUGqX XXXF


of 317

2.3.15 “25/50/25” Open-Hole Tension 1 Properties (OHT1)

Material:



Ply count: 16




No. Specimens

No. Prepreg Lots

21

3

CUGDX XXXA

21

3

7

1

Equilbrium

160 F,85%

CUGDX XXXD CUGDX XXXF

OHT1 Strength [ksi]

CTD

-65

Dry

CUGDX XXXB

21

3

Source code




Equilbrium at T, RH

RTD

70

Dry

Open-Hole Tension 1Cytec 5320-1 T650 Unitape Gr 145 RC 33%

[45/0/-45/90]2S

ETW2

250

Equilbrium

160 F,85%

ETW1

180


of 317


Material:



Ply count: 20




No. Specimens

No. Prepreg Lots

70

Dry

OHT2 Strength [ksi]

21

3



Equilbrium at T, RH

Source code

CTD

-65

Dry

CUGEX XXXB

21

3


[45/-45/0/45/-45/90/45/-45/45/-45]S

CUGEX XXXA

21

3

ETW2

250

Equilbrium

160 F,85%

CUGEX XXXF


RTD


of 317


Material:



Ply count: 20




No. Specimens

No. Prepreg Lots

22

3


[0/45/0/90/0/-45/0/45/0/-45]S

CUGFX XXXA

21

3

ETW2

250

Equilbrium

160 F,85%

CUGFX XXXF


RTDCTD

-65

Dry

CUGFX XXXB

70

Dry

OHT3 Strength [ksi]

21

3



Equilbrium at T, RH

Source code


of 317

2.3.18 “25/50/25” Filled-Hole Tension 1 Properties (FHT1)

Material:



Ply count: 16




No. Specimens

No. Prepreg Lots

21

3

CUG4X XXXA

21

3

7

1

Equilbrium

160 F,85%

CUG4X XXXD CUG4X XXXF

FHT1 Strength [ksi]

CTD

-65

Dry

CUG4X XXXB

21

3

Source code




Equilbrium at T, RH

RTD

70

Dry

Filled-Hole Tension 1Cytec 5320-1 T650 Unitape Gr 145 RC 33%

[45/0/-45/90]2S

ETW2

250

Equilbrium

160 F,85%

ETW1

180


of 317


Material:



Ply count: 20




No. Specimens

No. Prepreg Lots

70

Dry

FHT2 Strength [ksi]

20

3



Equilbrium at T, RH

Source code

CTD

-65

Dry

CUG5X XXXB

20

3


[45/-45/0/45/-45/90/45/-45/45/-45]S

CUG5X XXXA

20

3

ETW2

250

Equilbrium

160 F,85%

CUG5X XXXF


RTD


of 317


Material:



Ply count: 20




No. Specimens

No. Prepreg Lots

22

3


[0/45/0/90/0/-45/0/45/0/-45]S

CUG6X XXXA

21

3

ETW2

250

Equilbrium

160 F,85%

CUG6X XXXF


RTDCTD

-65

Dry

CUG6X XXXB

70

Dry

FHT3 Strength [ksi]

21

3



Equilbrium at T, RH

Source code


of 317

2.3.21 “25/50/25” Open-Hole Compression 1 Properties (OHC1)

Material:



Ply count: 32




No. Specimens

No. Prepreg Lots

21

3

Open-Hole Compression 1Cytec 5320-1 T650 Unitape Gr 145 RC 33%

[45/0/-45/90]4S

CUGGX XXXD

7

1

ETW2

250

Equilbrium

160 F,85%

CUGGX XXXF


ETW1RTD

70

Dry

CUGGX XXXA

180

Equilbrium

160 F,85%

OHC1 Strength [ksi]

21

3



Equilbrium at T, RH

Source code


of 317


Material:



Ply count: 40




No. Specimens

No. Prepreg Lots

21

3


Equilbrium at T, RH

OHC2 Strength [ksi]

3

Source code

Equilbrium

160 F,85%

CUGHX XXXF

Dry

21

CUGHX XXXA


[45/-45/0/45/-45/90/45/-45/45/-45]2S


ETW2


RTD

70


of 317


Material:



Ply count: 40




No. Specimens

No. Prepreg Lots


[0/45/0/90/0/-45/0/45/0/-45]2S


ETW2


RTD

70

Dry

22

CUGIX XXXA

21

3


Equilbrium at T, RH

OHC3 Strength [ksi]

3

Source code

Equilbrium

160 F,85%

CUGIX XXXF


of 317

2.3.24 “25/50/25” Filled-Hole Compression 1 Properties (FHC1)

Material:



Ply count: 32




No. Specimens

No. Prepreg Lots

180

Equilbrium

160 F,85%

FHC1 Strength [ksi]

21

3



Equilbrium at T, RH

Source code

RTD

70

Dry

CUG7X XXXA

21

3

Filled-Hole Compression 1Cytec 5320-1 T650 Unitape Gr 145 RC 33%

[45/0/-45/90]4S

CUG7X XXXD

7

1

ETW2

250

Equilbrium

160 F,85%

CUG7X XXXF


ETW1


of 317


Material:



Ply count: 40




No. Specimens

No. Prepreg Lots

21

3


Equilbrium at T, RH

FHC2 Strength [ksi]

3

Source code

Equilbrium

160 F,85%

CUG8X XXXF

Dry

21

CUG8X XXXA


[45/-45/0/45/-45/90/45/-45/45/-45]2S


ETW2


RTD

70


of 317


Material:



Ply count: 40




No. Specimens

No. Prepreg Lots

21

3


Equilbrium at T, RH

FHC3 Strength [ksi]

3

Source code

Equilbrium

160 F,85%

CUG9X XXXF

Dry

21

CUG9X XXXA


[0/45/0/90/0/-45/0/45/0/-45]2S


ETW2


RTD

70


of 317

2.3.27 “25/50/25” Single-Shear Bearing 1 Properties (SSB1)

Material:



Ply count: 16




No. Specimens

No. Prepreg Lots


No. Specimens

No. Prepreg Lots


No. Specimens

No. Prepreg Lots

Source code

ETW2

250

Equilbrium

160 F,85%

CUG1X XXXA




Equilbrium at T, RH

RTD

70

Dry

SSB1 Initial Peak Bearing Strength [ksi]

SSB1 2% Offset Strength [ksi]

SSB1 Ultimate Strength [ksi]

1

21

3

ETW1

180

Equilbrium

160 F,85%

CUG1X XXXD

7

1

18

3

21

3

7

1

7

3

21

3

Single-Shear Bearing 1Cytec 5320-1 T650 Unitape Gr 145 RC 33%

[45/0/-45/90]2S

CUG1X XXXF

21

3

21


of 317


Material:



Ply count: 20




No. Specimens

No. Prepreg Lots


No. Specimens

No. Prepreg Lots



Source code


[45/-45/0/45/-45/90/45/-45/45/-45]S




Equilbrium at T, RH

RTD

70

Dry

CUG2X XXXA

3

21

3

ETW2

250

Equilbrium

160 F,85%

CUG2X XXXF

21

3

21

3

21


of 317


Material:



Ply count: 20




No. Specimens

No. Prepreg Lots


No. Specimens

No. Prepreg Lots


No. Specimens

No. Prepreg Lots

21

3

21

3

22

3

ETW2

250

Equilbrium

160 F,85%

CUG3X XXXF

16

3

20

3

22

3

SSB3 Initial Peak Bearing Strength [ksi]



Source code


[0/45/0/90/0/-45/0/45/0/-45]S




Equilbrium at T, RH

RTD

70

Dry

CUG3X XXXA


of 317

2.3.30 Compression After Impact 1 Properties (CAI1)

Material:



Ply count: 32

Test method: ASTM D7136/7137-07


Normalized MeasuredMean 24.280 24.270Minimum 23.466 23.549Maximum 25.129 25.044C.V.(%) 2.633 2.374

No. SpecimensNo. Prepreg Lots




Equilbrium at T, RH

Compression After Impact 1Cytec 5320-1 T650 Unitape Gr 145 RC 33%

[45/0/-45/90]4S

CAI Strength [ksi]

RTD

70

Dry

CUGKX XXXA

71

Source code


of 317

2.3.31 Interlaminar Tension Properties (ILT)

Material:



Ply count: 30


Normalized by: NA

Normalized Measured Normalized Measured Normalized MeasuredMean 238.501 251.215 153.369Minimum 188.327 213.670 119.620Maximum 281.814 293.481 174.475C.V.(%) 14.934 10.991 12.320

No. Specimens

No. Prepreg Lots

Mean 6.831 7.399 4.719Minimum 5.416 6.106 3.502Maximum 8.110 8.597 5.489C.V.(%) 14.761 10.959 13.101

No. Specimens

No. Prepreg Lots




Equilbrium at T, RH

Interlaminar TensionCytec 5320-1 T650 Unitape Gr 145 RC 33%

[0]30

RTD

70

Dry

CBS [lb]

ILT [ksi]

CTD

-65

Dry

CUGMX XXXB

7

Source code

1

7

1

CUGMX XXXA

ETW2

250

Equilbrium

160 F,85%

CUGMX XXXF

1

7

1

7

1

8

1

8


of 317

3. Individual Test Charts

These charts combine all three batches of data and plot the minimum and maximum modulus and strength range based on the test temperature.


of 317

3.1 Longitudinal Tension Properties (LT)

0

50

100

150

200

250

300

350

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Longitudinal Tension (LT) Strength--NormalizedCytec 5320-1 T650 Unitape Gr 145 RC 33%

Dry Condition

Wet Condition

0

5

10

15

20

25

‐100 ‐50 0 50 100 150 200 250 300

Modulus [M

si]

Temperature [°F]

Longitudinal Tension (LT) Modulus--NormalizedCytec 5320-1 T650 Unitape Gr 145 RC 33%

Dry Condition

Wet Condition


of 317

3.2 Transverse Tension Properties (TT)

0

2

4

6

8

10

12

14

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Transverse Tension (TT) Strength--MeasuredCytec 5320-1 T650 Unitape Gr 145 RC 33%

Dry Condition

Wet Condition

0.0

0.2

0.4

0.6

0.8

1.0

1.2

1.4

1.6

1.8

‐100 ‐50 0 50 100 150 200 250 300

Modulus [M

si]

Temperature [°F]

Transverse Tension (TT) Modulus--MeasuredCytec 5320-1 T650 Unitape Gr 145 RC 33%

Dry Condition

Wet Condition


of 317

3.3 Longitudinal Compression Properties (LC)

0

5

10

15

20

25

‐100 ‐50 0 50 100 150 200 250 300

Modulus [M

si]

Temperature [°F]

Longitudinal Compression (LC) Modulus--Normalized


Dry Condition

Wet Condition


of 317

3.4 Transverse Compression Properties (TC)

0

10

20

30

40

50

60

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Transverse Compression (TC) Strength--MeasuredCytec 5320-1 T650 Unitape Gr 145 RC 33%

Dry Condition

Wet Condition

0.0

0.2

0.4

0.6

0.8

1.0

1.2

1.4

1.6

1.8

‐100 ‐50 0 50 100 150 200 250 300

Modulus [M

si]

Temperature [°F]

Transverse Compression (TC) Modulus--MeasuredCytec 5320-1 T650 Unitape Gr 145 RC 33%

Dry Condition

Wet Condition


of 317

3.5 In-Plane Shear Properties (IPS)

0

2

4

6

8

10

12

14

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

In-Plane Shear (IPS) Strength at 0.2% Offset--Measured


Dry Condition

Wet Condition

0

2

4

6

8

10

12

14

16

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

In-Plane Shear (IPS) Strength at 5% Strain--Measured


Dry Condition

Wet Condition


of 317

0.0

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

0.9

1.0

‐100 ‐50 0 50 100 150 200 250 300

Modulus [M

si]

Temperature [°F]

In-Plane Shear (IPS) Modulus--MeasuredCytec 5320-1 T650 Unitape Gr 145 RC 33%

Dry Condition

Wet Condition


of 317

3.6 “25/50/25” Unnotched Tension 1 Properties (UNT1)

0

20

40

60

80

100

120

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Laminate Unnotched Tension (UNT1) Strength--Normalized


Dry Condition

Wet Condition

0

1

2

3

4

5

6

7

8

9

‐100 ‐50 0 50 100 150 200 250 300

Modulus [M

si]

Temperature [°F]

Laminate Unnotched Tension (UNT1) Modulus--Normalized


Dry Condition

Wet Condition


of 317


0

10

20

30

40

50

60

70

80

90

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]



Dry Condition

Wet Condition

0

1

2

3

4

5

6

‐100 ‐50 0 50 100 150 200 250 300

Modulus [M

si]

Temperature [°F]



Dry Condition

Wet Condition


of 317


0

20

40

60

80

100

120

140

160

180

200

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]



Dry Condition

Wet Condition

0

2

4

6

8

10

12

14

‐100 ‐50 0 50 100 150 200 250 300

Modulus [M

si]

Temperature [°F]



Dry Condition

Wet Condition


of 317

3.9 “33/0/67” Unnotched Compression 0 Properties (UNC0)

0

20

40

60

80

100

120

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Laminate Unnotched Compression (UNC0) Strength--Normalized


Dry Condition

Wet Condition

0

1

2

3

4

5

6

7

8

‐100 ‐50 0 50 100 150 200 250 300

Modulus [M

si]

Temperature [°F]

Laminate Unnotched Compression (UNC0) Modulus--Normalized


Dry Condition

Wet Condition


of 317


0

20

40

60

80

100

120

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]



Dry Condition

Wet Condition

0

1

2

3

4

5

6

7

8

0 50 100 150 200 250 300

Modulus [M

si]

Temperature [°F]



Dry Condition

Wet Condition


of 317


0

10

20

30

40

50

60

70

80

90

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]



Dry Condition

Wet Condition

0

1

2

3

4

5

6

0 50 100 150 200 250 300

Modulus [M

si]

Temperature [°F]



Dry Condition

Wet Condition


of 317


0

20

40

60

80

100

120

140

160

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]



Dry Condition

Wet Condition

0

2

4

6

8

10

12

0 50 100 150 200 250 300

Modulus [M

si]

Temperature [°F]



Dry Condition

Wet Condition


of 317

3.13 Lamina Short-Beam Shear Properties (SBS)

0

5

10

15

20

25

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Short-Beam Strength (SBS) Strength--MeasuredCytec 5320-1 T650 Unitape Gr 145 RC 33%

Dry Condition

Wet Condition

3.14 Laminate Short-Beam Strength Properties (SBS1)

0

2

4

6

8

10

12

14

16

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Laminate Short-Beam Strength (SBS1) Strength--Measured


Dry Condition

Wet Condition


of 317

3.15 “25/50/25” Open-Hole Tension 1 Properties (OHT1)

0

10

20

30

40

50

60

70

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Laminate Open-Hole Tension (OHT1) Strength--Normalized


Dry Condition

Wet Condition


0

5

10

15

20

25

30

35

40

45

50

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]



Dry Condition

Wet Condition


of 317


0

10

20

30

40

50

60

70

80

90

100

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]



Dry Condition

Wet Condition

3.18 “25/50/25” Filled-Hole Tension 1 Properties (FHT1)

0

10

20

30

40

50

60

70

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Laminate Filled-Hole Tension (FHT1) Strength--Normalized


Dry Condition

Wet Condition


of 317


0

10

20

30

40

50

60

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]



Dry Condition

Wet Condition


0

10

20

30

40

50

60

70

80

90

100

‐100 ‐50 0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]



Dry Condition

Wet Condition


of 317

3.21 “25/50/25” Open-Hole Compression 1 Properties (OHC1)

0

10

20

30

40

50

60

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Laminate Open-Hole Compression (OHC1) Strength--Normalized


Dry Condition

Wet Condition


0

5

10

15

20

25

30

35

40

45

50

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]



Dry Condition

Wet Condition


of 317


0

10

20

30

40

50

60

70

80

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]



Dry Condition

Wet Condition

3.24 “25/50/25” Filled-Hole Compression 1 Properties (FHC1)

0

10

20

30

40

50

60

70

80

90

100

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Laminate Filled-Hole Compression (FHC1) Strength--Normalized


Dry Condition

Wet Condition


of 317


0

10

20

30

40

50

60

70

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]



Dry Condition

Wet Condition


0

20

40

60

80

100

120

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]



Dry Condition

Wet Condition


of 317

3.27 “25/50/25” Single-Shear Bearing Strength1 Properties (SSB1)

0

20

40

60

80

100

120

140

160

0 50 100 150 200 250 300

Initial Peak Bearing Strength [ksi]

Temperature [°F]

Laminate Single-Shear Bearing (SSB1) Initial Peak Bearing Strength--NormalizedCytec 5320-1 T650 Unitape Gr 145 RC 33%

Dry Condition

Wet Condition

0

20

40

60

80

100

120

140

160

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Laminate Single-Shear Bearing (SSB1) 2% Offset Strength--Normalized


Dry Condition

Wet Condition


of 317

0

20

40

60

80

100

120

140

160

180

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Laminate Single-Shear Bearing (SSB1) UltimateStrength--Normalized


Dry Condition

Wet Condition


of 317

3.28 “10/80/10” Single-Shear Bearing Strength 2 Properties (SSB2)

0

20

40

60

80

100

120

140

160

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Laminate Single-Shear Bearing (SSB2) 2% Offset Strength--Normalized


Dry Condition

Wet Condition

0

20

40

60

80

100

120

140

160

180

200

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Laminate Single-Shear Bearing (SSB2) UltimateStrength--Normalized


Dry Condition

Wet Condition


of 317

3.29 “50/40/10” Single-Shear Bearing 3 Properties (SSB3)

0

20

40

60

80

100

120

140

160

0 50 100 150 200 250 300

Initial Peak Bearing Strength [ksi]

Temperature [°F]

Laminate Single-Shear Bearing (SSB3) Initial Peak Bearing Strength--NormalizedCytec 5320-1 T650 Unitape Gr 145 RC 33%

Dry Condition

Wet Condition

0

20

40

60

80

100

120

140

160

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Laminate Single-Shear Bearing (SSB3) 2% OffsetStrength--Normalized


Dry Condition

Wet Condition


of 317

0

20

40

60

80

100

120

140

160

180

0 50 100 150 200 250 300

Strength [ksi]

Temperature [°F]

Laminate Single-Shear Bearing (SSB3) Ultimate Strength--Normalized


Dry Condition

Wet Condition

3.30 Compression After Impact 1 Properties (CAI1)

0

5

10

15

20

25

30

0 10 20 30 40 50 60 70 80

Strength [ksi]

Temperature [°F]

Laminate Compression After Impact (CAI1) Strength--Normalized


Dry Condition

Wet Condition


of 317

3.31 Interlaminar Tension Properties (ILT)

0

50

100

150

200

250

300

350

‐100 ‐50 0 50 100 150 200 250 300

CBS [lb]

Temperature [°F]

Curved Beam Strength (CBS)--MeasuredCytec 5320-1 T650 Unitape Gr 145 RC 33%

Dry Condition

Wet Condition

0

1

2

3

4

5

6

7

8

9

10

‐100 ‐50 0 50 100 150 200 250 300

ILT [ksi]

Temperature [°F]

Interlaminar Tension Strength (ILT)--MeasuredCytec 5320-1 T650 Unitape Gr 145 RC 33%

Dry Condition

Wet Condition


of 317

4. Raw Data

4.1 Longitudinal Tension Properties (LT)

normalizing tply [in]0.0055

Specimen Number

Cytec Batch #

Cytec Cure Cycle

Prepreg Lot # Cure Cycle # Strength [ksi]Modulus

[Msi]Poisson's

Ratio

Avg. Specimen Thickness

[in]

# Plies in Laminate

Failure Mode Avg. tply [in]Strengthnorm

[ksi]

Modulusnorm

[Msi]

CUGJD116B D C1 4 1 311.839 20.082 0.312 0.044 8 SGM / LGM 0.0055 309.123 19.907CUGJD117B D C1 4 1 305.584 20.454 0.324 0.044 8 SGM / LGM 0.0055 304.774 20.400CUGJD118B D C1 4 1 305.669 20.573 0.359 0.044 8 SGM / LGM 0.0054 302.196 20.339CUGJD119B D C1 4 1 287.991 20.323 0.329 0.044 8 SGM / LGM 0.0055 289.846 20.454CUGJD216B D C2 4 2 286.056 19.941 0.320 0.043 8 SGM 0.0053 277.387 19.337CUGJD217B D C2 4 2 297.938 20.188 0.361 0.043 8 SGM 0.0053 288.459 19.546CUGJD218B D C2 4 2 266.291 19.673 0.316 0.043 8 SGM 0.0054 260.542 19.248CUGJE117B E C1 5 1 286.684 20.402 0.337 0.044 8 SGM / LGM 0.0055 288.856 20.556CUGJE118B E C1 5 1 295.586 20.048 0.279 0.045 8 SGM / LGM 0.0057 304.319 20.640CUGJE119B E C1 5 1 285.512 19.831 0.316 0.045 8 SGM 0.0057 294.272 20.439CUGJE11AB E C1 5 1 294.575 19.702 0.308 0.045 8 SGM 0.0056 300.935 20.128CUGJE217B E C2 5 2 288.264 20.468 0.316 0.044 8 SGM / LGM 0.0055 288.701 20.499CUGJE218B E C2 5 2 278.361 19.913 0.309 0.045 8 SGM 0.0056 281.735 20.155CUGJE219B E C2 5 2 277.629 20.620 0.364 0.044 8 SGM 0.0055 278.575 20.691CUGJF117B F C1 6 1 297.491 19.842 0.344 0.044 8 SGM 0.0055 297.716 19.857CUGJF119B F C1 6 1 308.338 20.511 0.333 0.045 8 SGM 0.0056 313.945 20.884CUGJF11AB F C1 6 1 311.785 19.469 0.311 0.046 8 SGM / LGM 0.0057 323.949 20.228CUGJF11CB F C1 6 1 294.150 20.262 0.322 0.044 8 SGM / LGM 0.0054 290.919 20.040CUGJF217B F C2 6 2 300.770 19.903 0.320 0.045 8 SGM 0.0056 305.897 20.242CUGJF218B F C2 6 2 272.926 20.348 0.333 0.045 8 SGM 0.0056 277.681 20.702CUGJF219B F C2 6 2 285.220 20.146 0.300 0.044 8 SGM 0.0055 286.084 20.207

Average 292.317 20.128 0.325 Averagenorm 0.0055 293.615 20.214Standard Dev. 12.623 0.326 0.021 Standard Dev.norm 14.557 0.440

Coeff. of Var. [%] 4.318 1.619 6.384 Coeff. of Var. [%]norm 4.958 2.175Min. 266.291 19.469 0.279 Min. 0.0053 260.542 19.248Max. 311.839 20.620 0.364 Max. 0.0057 323.949 20.884

Number of Spec. 21 21 21 Number of Spec. 21 21 21

Longitudinal Tension Properties (LT)--CTDStrength & Modulus



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Longitudinal Tension Strength [ksi]

Longitudinal Tension Properties (LT)--CTDNormalized Strength


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Longitudinal Tension Modulus [Msi]

Longitudinal Tension Properties (LT)--CTDNormalized Modulus


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Prepreg Lot #


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Specimen Number

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Cytec Cure Cycle


[Msi]Poisson's

Ratio


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGJD112A* D C1 4 1 312.095 20.322 0.329 0.043 8 XGM 0.0054 305.121 19.868CUGJD113A* D C1 4 1 320.612 20.296 0.317 0.044 8 XGM 0.0055 321.341 20.342CUGJD114A D C1 4 1 313.751 20.220 0.317 0.044 8 XGM 0.0055 310.899 20.036CUGJD115A D C1 4 1 294.347 19.536 0.332 0.042 8 SGM 0.0053 281.525 18.685CUGJD211A D C2 4 2 316.185 20.298 0.323 0.045 8 LGM / SGM 0.0057 324.928 20.860CUGJD212A D C2 4 2 293.593 19.931 0.330 0.044 8 SGM 0.0055 295.038 20.029CUGJD213A D C2 4 2 290.111 19.785 0.330 0.044 8 LGM / SGM 0.0055 289.561 19.747CUGJE111A E C1 5 1 317.221 20.283 0.316 0.044 8 LGM / SGM 0.0055 314.697 20.122CUGJE112A E C1 5 1 306.859 20.152 0.319 0.044 8 SGM 0.0055 305.697 20.075CUGJE113A E C1 5 1 311.111 19.788 0.314 0.045 8 XGM 0.0056 318.771 20.275CUGJE114A E C1 5 1 302.033 20.163 0.341 0.044 8 SGM 0.0055 304.092 20.300CUGJE211A E C2 5 2 296.295 20.062 0.328 0.044 8 SGM 0.0055 297.642 20.153CUGJE212A E C2 5 2 305.782 20.106 0.317 0.044 8 XGM 0.0055 307.172 20.197CUGJE213A E C2 5 2 284.748 19.998 0.322 0.045 8 SGM 0.0056 288.092 20.233CUGJF111A F C1 6 1 275.142 20.695 0.371 0.044 8 XGM 0.0055 275.142 20.695CUGJF112A F C1 6 1 272.279 ** ** 0.044 8 SGM 0.0055 273.517CUGJF113A F C1 6 1 269.754 20.283 0.324 0.044 8 SGM 0.0056 272.717 20.506CUGJF114A F C1 6 1 281.776 19.801 0.323 0.044 8 SGM 0.0055 282.843 19.876CUGJF211A F C2 6 2 318.682 20.102 0.320 0.043 8 LGM / SGM 0.0054 312.163 19.691CUGJF212A F C2 6 2 300.246 19.914 0.320 0.044 8 SGM 0.0055 301.611 20.004CUGJF213A F C2 6 2 296.467 19.814 0.320 0.044 8 XGM 0.0055 298.376 19.941

* Strain measurement was measured with SG. Extensometer used on other coupons. ** Modulus and poisson's ratio not reported due to erroneous strain data.




Longitudinal Tension Properties (LT)--RTDStrength & Modulus



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Longitudinal Tension Properties (LT)--RTDNormalized Strength


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Longitudinal Tension Properties (LT)--RTDNormalized Modulus


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Specimen Number

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[Msi]Poisson's

Ratio


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGJD11BD D C1 4 1 272.164 20.735 0.385 0.043 8 XGM 0.0054 266.391 20.295CUGJD11CD D C1 4 1 248.616 * * 0.044 8 XGM 0.0055 246.355CUGJD11DD D C1 4 1 254.321 20.017 0.336 0.045 8 SGM 0.0056 257.211 20.245CUGJD11ED D C1 4 1 282.351 20.525 0.318 0.044 8 XGM 0.0055 280.960 20.424CUGJD11FD D C1 4 1 252.228 19.670 0.329 0.042 8 XGM 0.0053 241.145 18.806CUGJD21BD D C2 4 2 305.972 20.891 0.318 0.044 8 XGM 0.0054 303.075 20.693CUGJD21CD D C2 4 2 303.419 19.829 0.323 0.044 8 SGM 0.0055 303.649 19.844CUGJD21DD D C2 4 2 289.065 20.175 0.329 0.043 8 SGM / XGM 0.0054 285.123 19.900

* Modulus and poisson's ratio not reported due to erroneous strain data.




Longitudinal Tension Properties (LT)--ETW1Strength & Modulus



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Longitudinal Tension Properties (LT)--ETW1Normalized Strength


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Longitudinal Tension Properties (LT)--ETW1Normalized Modulus


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[Msi]Poisson's

Ratio


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGJD11GF D C1 4 1 255.897 20.075 0.302 0.044 8 XGM 0.0055 253.571 19.893CUGJD11HF D C1 4 1 258.052 * * 0.043 8 XGM / LGM 0.0054 254.240CUGJD11IF D C1 4 1 258.476 20.546 0.331 0.044 8 XGM / LWT 0.0055 257.889 20.500CUGJD11JF D C1 4 1 262.283 20.188 0.340 0.045 8 SGM / XGM 0.0056 265.263 20.418CUGJD11KF D C1 4 1 247.300 19.985 0.336 0.044 8 XGM 0.0056 249.923 20.197CUGJD21GF D C2 4 2 292.925 19.555 0.350 0.044 8 XGM 0.0055 290.262 19.377CUGJD21HF D C2 4 2 282.464 19.740 0.349 0.043 8 SGM / XGM 0.0054 274.760 19.202CUGJD21IF D C2 4 2 288.842 19.791 0.353 0.043 8 XGM 0.0054 282.386 19.349CUGJD21JF D C2 4 2 297.509 19.943 0.359 0.044 8 XGM 0.0056 300.326 20.132CUGJE11DF E C1 5 1 297.397 19.970 0.340 0.045 8 XGM 0.0057 306.071 20.553CUGJE11EF E C1 5 1 304.278 19.844 0.345 0.045 8 XGM 0.0056 312.116 20.355CUGJE11FF E C1 5 1 289.543 19.926 0.317 0.046 8 XGM 0.0057 300.840 20.703CUGJE11GF E C1 5 1 290.707 19.808 0.329 0.045 8 XGM 0.0056 298.085 20.311CUGJE21DF E C2 5 2 267.075 20.258 0.337 0.044 8 XGM 0.0055 268.693 20.381CUGJE21EF E C2 5 2 249.412 19.925 0.334 0.044 8 XGM 0.0056 251.963 20.129CUGJE21FF E C2 5 2 257.676 20.357 0.347 0.044 8 XGM 0.0056 260.507 20.581CUGJF11DF F C1 6 1 234.705 19.624 0.344 0.044 8 XGM 0.0056 236.839 19.802CUGJF11EF F C1 6 1 257.487 19.593 0.337 0.045 8 SGM / XGM 0.0056 263.047 20.016CUGJF11FF F C1 6 1 247.064 19.597 0.317 0.045 8 XGM 0.0057 254.364 20.176CUGJF11GF F C1 6 1 234.704 19.354 0.322 0.045 8 SGM 0.0056 238.171 19.640CUGJF21DF F C2 6 2 294.329 19.831 0.344 0.045 8 XGM 0.0056 298.342 20.102CUGJF21EF F C2 6 2 292.158 19.665 0.334 0.044 8 XGM 0.0056 294.814 19.844CUGJF21FF F C2 6 2 297.312 20.054 0.339 0.044 8 XGM 0.0055 299.452 20.198

* Modulus and poisson's ratio not reported due to erroneous strain data.




Longitudinal Tension Properties (LT)--ETW2Strength & Modulus



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4.2 Transverse Tension Properties (TT)

Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate

Failure Mode Avg. tply [in]

CUGUD116B D C1 4 1 11.863 1.464 0.087 16 LAT 0.0055CUGUD117B D C1 4 1 12.078 1.446 0.088 16 LAT 0.0055CUGUD118B D C1 4 1 11.423 1.475 0.088 16 LAT 0.0055CUGUD119B D C1 4 1 11.953 1.462 0.088 16 LAB 0.0055CUGUD216B D C2 4 2 11.909 1.477 0.088 16 LAB 0.0055CUGUD217B D C2 4 2 11.806 1.518 0.087 16 LAB 0.0054CUGUD218B D C2 4 2 12.167 1.564 0.087 16 LAB 0.0054CUGUE117B E C1 5 1 11.713 1.462 0.089 16 LAT 0.0056CUGUE118B E C1 5 1 11.569 1.472 0.088 16 LAT 0.0055CUGUE119B E C1 5 1 10.944 1.478 0.088 16 LAB 0.0055CUGUE11AB E C1 5 1 10.220 1.568 0.089 16 LAB 0.0055CUGUE216B E C2 5 2 9.673 1.501 0.087 16 LGM 0.0054CUGUE217B E C2 5 2 9.405 1.561 0.087 16 LGM 0.0055CUGUE218B E C2 5 2 9.761 1.577 0.088 16 LGM 0.0055CUGUF117B F C1 6 1 7.610 1.415 0.089 16 LAT 0.0055CUGUF118B F C1 6 1 10.723 1.473 0.088 16 LAT 0.0055CUGUF119B F C1 6 1 7.718 1.497 0.087 16 LAB 0.0054CUGUF11AB F C1 6 1 11.866 1.443 0.088 16 LAB 0.0055CUGUF11BB* F C1 6 1 11.830 0.088 16 LAB 0.0055CUGUF11CB* F C1 6 1 13.142 0.088 16 LAB 0.0055CUGUF216B F C2 6 2 8.985 1.460 0.089 16 LAB 0.0055CUGUF217B F C2 6 2 12.724 1.421 0.088 16 LAT 0.0055CUGUF218B F C2 6 2 10.956 1.444 0.088 16 LAB 0.0055CUGUF219B* F C2 6 2 11.373 0.089 16 LAB 0.0055

*Specimen was not gaged

Average 10.975 1.485 Average 0.0055Standard Dev. 1.454 0.048 Standard Dev.

Coeff. of Var. [%] 13.251 3.218 Coeff. of Var. [%]Min. 7.610 1.415 Min. 0.0054Max. 13.142 1.577 Max. 0.0056

Number of Spec. 24 21 Number of Spec. 24

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Transverse Tension Properties (TT)--CTDMeasured Strength


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Transverse Tension Properties (TT)--CTDMeasured Modulus


Cure Cycle #

Prepreg Lot #


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Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


CUGUD111A* D C1 4 1 10.439 1.365 0.085 16 LGM 0.0053CUGUD112A* D C1 4 1 10.010 1.341 0.087 16 LGM 0.0054CUGUD113A D C1 4 1 11.202 1.315 0.088 16 LAT 0.0055CUGUD114A D C1 4 1 11.459 1.311 0.088 16 LAT 0.0055CUGUD211A D C2 4 2 8.171 1.403 0.084 16 LAB 0.0052CUGUD212A D C2 4 2 9.553 1.361 0.086 16 LAT 0.0054CUGUD213A D C2 4 2 8.772 1.331 0.087 16 LAB 0.0054CUGUE111A E C1 5 1 9.716 1.336 0.087 16 LAT 0.0055CUGUE112A E C1 5 1 10.639 1.339 0.088 16 LAT 0.0055CUGUE113A E C1 5 1 9.798 1.347 0.088 16 LAB 0.0055CUGUE114A E C1 5 1 9.349 1.343 0.088 16 LAB 0.0055CUGUE211A E C2 5 2 9.728 1.326 0.088 16 LAB 0.0055CUGUE212A E C2 5 2 10.505 1.324 0.088 16 LAB 0.0055CUGUE213A E C2 5 2 10.398 1.324 0.087 16 LGM 0.0055CUGUF111A F C1 6 1 11.219 1.291 0.089 16 LGM 0.0055CUGUF112A F C1 6 1 11.002 1.320 0.087 16 LGM 0.0054CUGUF113A F C1 6 1 10.470 1.308 0.088 16 LAB 0.0055CUGUF114A F C1 6 1 9.961 1.315 0.087 16 LAB 0.0054CUGUF211A F C2 6 2 9.772 1.324 0.087 16 LAT 0.0055CUGUF212A F C2 6 2 10.346 1.316 0.088 16 LAB 0.0055CUGUF213A F C2 6 2 9.508 1.300 0.088 16 LAB 0.0055

* Strain measurement was measured with SG. Extensometer used on other coupons.




Transverse Tension Properties (TT)--RTDStrength & Modulus



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Transverse Tension Properties (TT)--RTDMeasured Modulus


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Specimen Number

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Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


CUGUD11BD D C1 4 1 8.656 1.202 0.087 16 LGM 0.0055CUGUD11FD D C1 4 1 7.083 1.178 0.088 16 LAB 0.0055CUGUD21BD D C2 4 2 8.764 1.241 0.087 16 LWT 0.0054CUGUD21CD D C2 4 2 8.643 1.205 0.087 16 LWT 0.0055CUGUD21DD D C2 4 2 8.354 1.223 0.087 16 LWB 0.0054CUGUD21ED D C2 4 2 8.677 1.205 0.087 16 LGM 0.0055CUGUD21FD D C2 4 2 8.844 1.236 0.087 16 LWT 0.0055




Transverse Tension Properties (TT)--ETW1Strength & Modulus



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Transverse Tension Properties (TT)--ETW1Measured Strength


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Transverse Tension Properties (TT)--ETW1Measured Modulus


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Specimen Number

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[Msi]


[in]

# Plies in Laminate


CUGUD11GF D C1 4 1 5.960 0.843 0.088 16 LGM 0.0055CUGUD11HF D C1 4 1 5.469 0.870 0.088 16 LGM 0.0055CUGUD11IF D C1 4 1 5.345 0.852 0.088 16 LGM 0.0055CUGUD11JF D C1 4 1 4.722 0.844 0.087 16 LGM 0.0055

CUGUD11CF* D C1 4 1 4.521 0.836 0.088 16 LGM 0.0055CUGUD11DF* D C1 4 1 4.426 0.818 0.087 16 LGM 0.0055CUGUD11EF* D C1 4 1 5.151 0.860 0.088 16 LGM 0.0055CUGUD21GF D C2 4 2 5.072 0.860 0.087 16 LGM 0.0055CUGUD21HF D C2 4 2 5.183 0.874 0.086 16 LGM 0.0054CUGUD21IF D C2 4 2 5.134 0.860 0.088 16 LGM 0.0055CUGUE11DF E C1 5 1 4.183 0.835 0.089 16 LGM 0.0055CUGUE11EF E C1 5 1 4.782 0.851 0.088 16 LWB 0.0055CUGUE11FF E C1 5 1 4.407 0.837 0.089 16 LWT 0.0055CUGUE11GF E C1 5 1 4.529 0.835 0.088 16 LGM 0.0055CUGUE21BF E C2 5 2 3.607 0.831 0.088 16 LGM 0.0055CUGUE21CF E C2 5 2 3.546 0.869 0.088 16 LGM 0.0055CUGUE21DF E C2 5 2 4.025 0.821 0.088 16 LGM 0.0055CUGUF11DF F C1 6 1 4.443 0.804 0.088 16 LGM 0.0055CUGUF11EF F C1 6 1 4.636 0.814 0.088 16 LGM 0.0055CUGUF11FF F C1 6 1 4.410 0.811 0.087 16 LGM 0.0055CUGUF11GF F C1 6 1 4.999 0.853 0.088 16 LWT 0.0055CUGUF21BF F C2 6 2 5.465 0.814 0.089 16 LGM 0.0055CUGUF21CF F C2 6 2 5.046 0.844 0.089 16 LGM 0.0055CUGUF21DF F C2 6 2 4.463 0.829 0.089 16 LGM 0.0056

* Coupons are from 180F set but was accidentally tested at 250F




Transverse Tension Properties (TT)--ETW2Strength & Modulus



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4.3 Longitudinal Compression Properties (LC)


Specimen Number

Cytec Batch #

Cytec Cure Cycle

Prepreg Lot # Cure Cycle #Modulus

[Msi]


[in]

# Plies in Laminate

Avg. tply [in]Modulusnorm

[Msi]

CUGLD117B D C1 4 1 17.192 0.112 20 0.0056 17.442CUGLD118B D C1 4 1 15.000 0.112 20 0.0056 15.261CUGLD119B D C1 4 1 16.372 0.110 20 0.0055 16.417CUGLD11AB D C1 4 1 19.344 0.111 20 0.0056 19.575CUGLD216B D C2 4 2 17.121 0.107 20 0.0053 16.596CUGLD217B D C2 4 2 22.407 0.108 20 0.0054 21.898CUGLD218B D C2 4 2 17.198 0.109 20 0.0054 16.998CUGLE117B E C1 5 1 16.789 0.109 20 0.0055 16.680CUGLE118B E C1 5 1 16.801 0.108 20 0.0054 16.490CUGLE119B E C1 5 1 19.928 0.109 20 0.0055 19.828CUGLE11AB E C1 5 1 15.658 0.110 20 0.0055 15.649CUGLE216B E C2 5 2 15.261 0.110 20 0.0055 15.232CUGLE217B E C2 5 2 17.607 0.109 20 0.0054 17.371CUGLE218B E C2 5 2 17.238 0.107 20 0.0054 16.774CUGLF116B F C1 6 1 16.871 0.110 20 0.0055 16.920CUGLF117B F C1 6 1 17.374 0.110 20 0.0055 17.399CUGLF118B F C1 6 1 19.527 0.110 20 0.0055 19.583CUGLF119B F C1 6 1 18.478 0.111 20 0.0055 18.596CUGLF216B F C2 6 2 16.411 0.111 20 0.0055 16.496CUGLF217B F C2 6 2 15.855 0.111 20 0.0055 15.944CUGLF218B F C2 6 2 15.032 0.112 20 0.0056 15.236

Average 17.308 Averagenorm 0.0055 17.256Standard Dev. 1.808 Standard Dev.norm 1.737

Coeff. of Var. [%] 10.447 Coeff. of Var. [%]norm 10.064Min. 15.000 Min. 0.0053 15.232Max. 22.407 Max. 0.0056 21.898

Number of Spec. 21 Number of Spec. 21 21

Longitudinal Compression Properties (LC)--CTDModulus



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Longitudinal Compression Properties (LC)--CTDNormalized Modulus


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Prepreg Lot #


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Specimen Number

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[Msi]


[in]

# Plies in Laminate


[Msi]

CUGLD112A D C1 4 1 18.352 0.111 20 0.0055 18.443CUGLD113A D C1 4 1 17.916 0.111 20 0.0055 18.042CUGLD114A D C1 4 1 18.248 0.112 20 0.0056 18.507CUGLD115A D C1 4 1 18.023 0.112 20 0.0056 18.383CUGLD211A D C2 4 2 18.322 0.111 20 0.0056 18.559CUGLD212A D C2 4 2 17.950 0.109 20 0.0055 17.866CUGLD213A D C2 4 2 18.289 0.110 20 0.0055 18.270CUGLE111A E C1 5 1 18.659 0.108 20 0.0054 18.273CUGLE112A E C1 5 1 18.513 0.107 20 0.0054 18.067CUGLE113A E C1 5 1 18.592 0.110 20 0.0055 18.512CUGLE114A E C1 5 1 18.767 0.110 20 0.0055 18.741CUGLE211A E C2 5 2 18.572 0.107 20 0.0054 18.076CUGLE212A E C2 5 2 19.023 0.107 20 0.0053 18.459CUGLE213A E C2 5 2 18.752 0.107 20 0.0054 18.257CUGLF111A F C1 6 1 18.204 0.109 20 0.0054 18.014CUGLF112A F C1 6 1 18.382 0.110 20 0.0055 18.456CUGLF113A F C1 6 1 18.332 0.110 20 0.0055 18.386CUGLF114A F C1 6 1 18.287 0.111 20 0.0056 18.485CUGLF211A F C2 6 2 17.868 0.110 20 0.0055 17.791CUGLF212A F C2 6 2 18.131 0.111 20 0.0056 18.360CUGLF213A F C2 6 2 18.307 0.110 20 0.0055 18.373




Longitudinal Compression Properties (LC)--RTDModulus



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Cure Cycle #


Longitudinal Compression Properties (LC)--RTDNormalized Modulus


Cure Cycle #

Prepreg Lot #


of 317


Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[Msi]

CUGLF11BC F C1 6 1 18.377 0.110 20 0.0055 18.400CUGLF11CC F C1 6 1 18.319 0.110 20 0.0055 18.304CUGLF11EC F C1 6 1 18.445 0.110 20 0.0055 18.491CUGLF11KC F C1 6 1 18.615 0.110 20 0.0055 18.646CUGLF21BC F C2 6 2 18.318 0.111 20 0.0055 18.413CUGLF21CC F C2 6 2 18.528 0.110 20 0.0055 18.579CUGLF21DC F C2 6 2 18.247 0.111 20 0.0055 18.348




Longitudinal Compression Properties (LC)--ETD1Modulus



of 317

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Prepreg Lot #

Cure Cycle #


Longitudinal Compression Properties (LC)--ETD1Normalized Modulus


Cure Cycle #

Prepreg Lot #


of 317


Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[Msi]

CUGLF131D F C1 6 1 19.573 0.109 20 0.0054 19.312CUGLF132D F C1 6 1 18.281 0.110 20 0.0055 18.354CUGLF133D F C1 6 1 18.473 0.110 20 0.0055 18.536CUGLF134D F C1 6 1 18.347 0.111 20 0.0055 18.434CUGLF231D F C2 6 2 18.094 0.109 20 0.0054 17.895CUGLF232D F C2 6 2 18.484 0.110 20 0.0055 18.535CUGLF233D F C2 6 2 18.595 0.110 20 0.0055 18.669




Longitudinal Compression Properties (LC)--ETW1Modulus



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Cure Cycle #


Longitudinal Compression Properties (LC)--ETW1Normalized Modulus


Cure Cycle #

Prepreg Lot #


of 317


Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[Msi]

CUGLF11DE F C1 6 1 18.058 0.110 20 0.0055 18.126CUGLF11HE F C1 6 1 18.204 0.109 20 0.0055 18.119CUGLF11IE F C1 6 1 18.208 0.110 20 0.0055 18.274CUGLF11JE F C1 6 1 18.276 0.110 20 0.0055 18.339CUGLF21GE F C2 6 2 18.288 0.110 20 0.0055 18.355CUGLF21HE F C2 6 2 18.202 0.110 20 0.0055 18.278CUGLF21IE F C2 6 2 18.303 0.111 20 0.0055 18.409




Longitudinal Compression Properties (LC)--ETD2Modulus



of 317

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Cure Cycle #


Longitudinal Compression Properties (LC)--ETD2Normalized Modulus


Cure Cycle #

Prepreg Lot #


of 317


Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[Msi]

CUGLD11DF D C1 4 1 17.257 0.111 20 0.0056 17.472CUGLD11EF D C1 4 1 17.701 0.112 20 0.0056 18.019CUGLD11FF D C1 4 1 17.551 0.112 20 0.0056 17.842CUGLD11GF D C1 4 1 17.478 0.111 20 0.0056 17.655CUGLD21BF D C2 4 2 18.382 0.108 20 0.0054 17.990CUGLD21CF D C2 4 2 18.440 0.110 20 0.0055 18.438CUGLD21DF D C2 4 2 18.102 0.109 20 0.0055 17.999CUGLE11DF E C1 5 1 18.750 0.112 20 0.0056 19.068CUGLE11EF E C1 5 1 18.608 0.110 20 0.0055 18.602CUGLE11FF E C1 5 1 18.015 0.110 20 0.0055 18.050CUGLE11GF E C1 5 1 18.458 0.112 20 0.0056 18.740CUGLE21BF E C2 5 2 19.083 0.107 20 0.0054 18.606CUGLE21CF E C2 5 2 18.633 0.109 20 0.0054 18.436CUGLE21DF E C2 5 2 18.563 0.108 20 0.0054 18.261CUGLF137F F C1 6 1 18.482 0.109 20 0.0055 18.360CUGLF138F F C1 6 1 17.093 0.111 20 0.0055 17.198CUGLF139F F C1 6 1 18.167 0.111 20 0.0056 18.354CUGLF13AF F C1 6 1 18.529 0.111 20 0.0055 18.651CUGLF236F F C2 6 2 18.260 0.111 20 0.0055 18.366CUGLF237F F C2 6 2 18.548 0.111 20 0.0055 18.643CUGLF238F F C2 6 2 18.430 0.111 20 0.0055 18.544




Longitudinal Compression Properties (LC)--ETW2Modulus



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Longitudinal Compression Properties (LC)--ETW2Normalized Modulus


Cure Cycle #

Prepreg Lot #


of 317

4.4 Transverse Compression Properties (TC)

Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


CUGZD117B D C1 4 1 52.496 1.576 0.110 20 BGM 0.0055CUGZD118B D C1 4 1 51.727 1.519 0.110 20 BGM 0.0055CUGZD119B D C1 4 1 53.055 1.511 0.109 20 BGM 0.0055CUGZD11AB D C1 4 1 53.252 1.550 0.109 20 BGM 0.0055CUGZD216B D C2 4 2 53.788 1.551 0.110 20 BGM 0.0055CUGZD217B D C2 4 2 53.802 1.497 0.109 20 BGM 0.0055CUGZD218B D C2 4 2 51.208 1.562 0.109 20 BGM 0.0054CUGZE117B E C1 5 1 51.889 1.514 0.112 20 BGM 0.0056CUGZE118B E C1 5 1 46.520 1.523 0.112 20 BGM 0.0056CUGZE119B E C1 5 1 51.110 1.496 0.111 20 BGM 0.0056CUGZE11AB E C1 5 1 51.551 1.565 0.112 20 BGM 0.0056CUGZE216B E C2 5 2 51.888 1.583 0.109 20 BGM 0.0055CUGZE217B E C2 5 2 49.465 1.530 0.109 20 BGM 0.0055CUGZE218B E C2 5 2 50.658 1.561 0.109 20 BGM 0.0054CUGZF117B F C1 6 1 47.244 1.516 0.111 20 BGM 0.0056CUGZF118B F C1 6 1 53.272 1.485 0.112 20 BGM 0.0056CUGZF119B F C1 6 1 51.489 1.561 0.111 20 BGM 0.0056CUGZF11AB F C1 6 1 47.263 1.515 0.111 20 BGM 0.0056CUGZF216B F C2 6 2 53.834 1.518 0.110 20 BGM 0.0055CUGZF217B F C2 6 2 51.138 1.509 0.111 20 BGM 0.0055CUGZF218B F C2 6 2 52.681 1.507 0.111 20 BGM 0.0055




Transverse Compression Properties (TC)--CTDStrength & Modulus



of 317

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Cure Cycle #

Transverse Compression Strength [ksi]

Transverse Compression Properties (TC)--CTDMeasured Strength


Cure Cycle #

Prepreg Lot #

3

4

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6

7

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0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8

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Cure Cycle #

Transverse Compression Modulus [Msi]

Transverse Compression Properties (TC)--CTDMeasured Modulus


Cure Cycle #

Prepreg Lot #


of 317

Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


CUGZD111A D C1 4 1 39.507 1.451 0.103 20 BGM 0.0052CUGZD112A D C1 4 1 40.200 1.377 0.109 20 BGM 0.0054CUGZD113A D C1 4 1 40.109 1.353 0.109 20 BGM 0.0055CUGZD114A D C1 4 1 40.767 1.389 0.109 20 BGM 0.0055CUGZD211A D C2 4 2 37.936 1.536 0.104 20 BGM 0.0052CUGZD212A D C2 4 2 39.782 1.450 0.109 20 BGM 0.0055CUGZD213A D C2 4 2 40.096 1.422 0.109 20 BGM 0.0054CUGZE112A E C1 5 1 40.570 1.394 0.112 20 BGM 0.0056CUGZE113A E C1 5 1 41.323 1.395 0.112 20 BGM 0.0056CUGZE114A E C1 5 1 40.071 1.400 0.112 20 BGM 0.0056CUGZE115A E C1 5 1 40.970 1.389 0.112 20 BGM 0.0056CUGZE211A E C2 5 2 35.507 1.646 0.102 20 BGM 0.0051CUGZE212A E C2 5 2 39.959 1.485 0.109 20 BGM 0.0054CUGZE213A E C2 5 2 40.673 1.460 0.109 20 BGM 0.0054CUGZE214A* E C2 5 2 40.939 0.110 20 BGM 0.0055CUGZF111A F C1 6 1 40.525 1.390 0.110 20 BGM 0.0055CUGZF112A F C1 6 1 39.336 1.391 0.112 20 BGM 0.0056CUGZF113A F C1 6 1 39.593 1.382 0.111 20 BGM 0.0056CUGZF114A F C1 6 1 41.579 1.376 0.111 20 BGM 0.0056CUGZF211A F C2 6 2 36.012 1.468 0.103 20 BGM 0.0051CUGZF212A F C2 6 2 38.890 1.416 0.111 20 BGM 0.0055CUGZF213A F C2 6 2 41.529 1.404 0.110 20 BGM 0.0055CUGZF214A* F C2 6 2 38.401 0.112 20 BGM 0.0056*Specimen was not gaged




Transverse Compression Properties (TC)--RTDStrength & Modulus



of 317

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Cure Cycle #


Transverse Compression Properties (TC)--RTDMeasured Strength


Cure Cycle #

Prepreg Lot #

3

4

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6

7

0

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0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6 1.8

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Transverse Compression Properties (TC)--RTDMeasured Modulus


Cure Cycle #

Prepreg Lot #


of 317

Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


CUGZF11DC F C1 6 1 28.982 1.353 0.104 20 BAB 0.0052CUGZF11EC F C1 6 1 30.161 1.274 0.113 20 BGM 0.0056CUGZF11FC F C1 6 1 31.835 1.299 0.111 20 BGM 0.0056CUGZF11HC F C1 6 1 31.370 1.279 0.112 20 BGM 0.0056CUGZF21BC F C2 6 2 30.760 1.307 0.110 20 BGM 0.0055CUGZF21CC F C2 6 2 33.144 1.297 0.110 20 BGM 0.0055CUGZF21DC F C2 6 2 31.737 1.298 0.111 20 BGM 0.0055




Transverse Compression Properties (TC)--ETD1Strength & Modulus



of 317

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Cure Cycle #


Transverse Compression Properties (TC)--ETD1Measured Strength


Cure Cycle #

Prepreg Lot #

3

4

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6

7

0

1

2

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0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6

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Cure Cycle #


Transverse Compression Properties (TC)--ETD1Measured Modulus


Cure Cycle #

Prepreg Lot #


of 317

Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


CUGZF131D F C1 6 1 1.249 0.111 20 BGM 0.0055CUGZF132D F C1 6 1 1.289 0.110 20 BGM 0.0055CUGZF133D F C1 6 1 1.301 0.110 20 HGM 0.0055CUGZF134D F C1 6 1 1.271 0.110 20 BGM 0.0055CUGZF135D F C1 6 1 26.262 0.111 20 HGM 0.0055CUGZF136D F C1 6 1 25.752 0.111 20 BGM / BAT 0.0055CUGZF137D F C1 6 1 24.457 0.111 20 BAT 0.0055CUGZF138D F C1 6 1 25.586 0.111 20 BGM 0.0055CUGZF231D F C2 6 2 1.373 0.104 20 BGM 0.0052CUGZF232D F C2 6 2 1.296 0.110 20 BGM 0.0055CUGZF233D F C2 6 2 1.265 0.111 20 BGM 0.0055CUGZF234D F C2 6 2 24.657 0.111 20 BGM 0.0055CUGZF235D F C2 6 2 25.322 0.111 20 HGM 0.0056CUGZF236D F C2 6 2 24.584 0.111 20 BGM 0.0056




Transverse Compression Properties (TC)--ETW1Strength & Modulus



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Cure Cycle #


Transverse Compression Properties (TC)--ETW1Measured Strength


Cure Cycle #

Prepreg Lot #

3

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5

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7

0

1

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0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4 1.6

Prepreg Lot #

Cure Cycle #


Transverse Compression Properties (TC)--ETW1Measured Modulus


Cure Cycle #

Prepreg Lot #


of 317

Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


CUGZF11JE F C1 6 1 24.300 1.237 0.111 20 BGM 0.0056CUGZF11KE F C1 6 1 26.228 1.230 0.112 20 BGM 0.0056CUGZF11LE F C1 6 1 26.370 1.242 0.112 20 BGM 0.0056CUGZF11ME F C1 6 1 26.563 1.221 0.111 20 BGM 0.0056CUGZF21GE F C2 6 2 25.807 1.276 0.111 20 BGM 0.0056CUGZF21HE F C2 6 2 27.387 1.255 0.110 20 BGM 0.0055CUGZF21IE F C2 6 2 27.081 1.246 0.111 20 BGM 0.0055




Transverse Compression Properties (TC)--ETD2Strength & Modulus



of 317

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Cure Cycle #


Transverse Compression Properties (TC)--ETD2Measured Strength


Cure Cycle #

Prepreg Lot #

3

4

5

6

7

0

1

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0.0 0.2 0.4 0.6 0.8 1.0 1.2 1.4

Prepreg Lot #

Cure Cycle #


Transverse Compression Properties (TC)--ETD2Measured Modulus


Cure Cycle #

Prepreg Lot #


of 317

Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


CUGZD11DF D C1 4 1 1.169 0.105 20 BGM 0.0052CUGZD11EF D C1 4 1 1.194 0.109 20 HGM 0.0054CUGZD11FF D C1 4 1 1.128 0.110 20 BGM 0.0055CUGZD11GF D C1 4 1 1.162 0.109 20 BGM / TAT 0.0055CUGZD11HF D C1 4 1 19.821 0.110 20 HGM 0.0055CUGZD11IF D C1 4 1 19.354 0.109 20 BGM 0.0055CUGZD11JF D C1 4 1 18.794 0.110 20 BGM 0.0055CUGZD11KF D C1 4 1 18.752 0.110 20 HGM 0.0055CUGZD21BF D C2 4 2 1.025 0.109 20 HGM 0.0055CUGZD21CF D C2 4 2 1.077 0.109 20 BGM 0.0054CUGZD21DF D C2 4 2 1.093 0.108 20 BGM / TAB 0.0054CUGZD21EF D C2 4 2 19.734 0.109 20 BGM 0.0054CUGZD21FF D C2 4 2 19.332 0.109 20 HGM / TAT 0.0054CUGZD21GF D C2 4 2 19.465 0.109 20 HGM 0.0054CUGZE11DF E C1 5 1 1.176 0.103 20 BGM / TAT 0.0051CUGZE11EF E C1 5 1 1.129 0.110 20 HGM 0.0055CUGZE11FF E C1 5 1 1.098 0.111 20 HGM 0.0056CUGZE11GF E C1 5 1 1.184 0.111 20 BGM 0.0056CUGZE11HF E C1 5 1 19.987 0.110 20 TAT / HGM 0.0055CUGZE11IF E C1 5 1 20.350 0.111 20 BGM 0.0056CUGZE11JF E C1 5 1 19.278 0.111 20 BGM 0.0056CUGZE11KF E C1 5 1 19.364 0.111 20 BGM 0.0056CUGZE21BF E C2 5 2 1.119 0.109 20 HGM / TAT 0.0055CUGZE21CF E C2 5 2 1.108 0.109 20 BGM 0.0055CUGZE21DF E C2 5 2 1.103 0.109 20 BGM / TAT 0.0055CUGZE21EF E C2 5 2 18.975 0.109 20 BGM 0.0055CUGZE21FF E C2 5 2 18.859 0.109 20 BGM 0.0055CUGZE21GF E C2 5 2 18.232 0.109 20 HGM 0.0055CUGZF13DF F C1 6 1 0.999 0.112 20 BGM 0.0056CUGZF13EF F C1 6 1 1.020 0.112 20 HGM / TAT 0.0056CUGZF13FF F C1 6 1 1.022 0.111 20 HGM / TAT 0.0055CUGZF13GF F C1 6 1 1.026 0.112 20 BGM 0.0056CUGZF13HF F C1 6 1 18.430 0.113 20 BGM 0.0056CUGZF13IF F C1 6 1 19.189 0.112 20 BGM 0.0056CUGZF13JF F C1 6 1 19.216 0.112 20 BGM 0.0056CUGZF13KF F C1 6 1 19.832 0.111 20 HGM 0.0056CUGZF23BF F C2 6 2 1.057 0.111 20 HGM 0.0056CUGZF23CF F C2 6 2 1.053 0.111 20 BGM 0.0055CUGZF23DF F C2 6 2 1.027 0.111 20 BGM 0.0056CUGZF23EF F C2 6 2 20.039 0.110 20 BGM / TAB 0.0055CUGZF23FF F C2 6 2 20.164 0.111 20 BGM 0.0056CUGZF23GF F C2 6 2 19.472 0.111 20 BGM 0.0056




Transverse Compression Properties (TC)--ETW2Strength & Modulus



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Transverse Compression Properties (TC)--ETW2Measured Strength


Cure Cycle #

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Transverse Compression Properties (TC)--ETW2Measured Modulus


Cure Cycle #

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of 317

4.5 In-Plane Shear Properties (IPS)

Specimen Number

Cytec Batch #Cytec Cure

CyclePrepreg Lot # Cure Cycle #

0.2% Offset Strength [ksi]

Peak Shear Strength

before 5% Strain [ksi]

Modulus [Msi]


[in]

# Plies in Laminate

Avg. tply [in]

CUGND115B D C1 4 1 11.394 17.483 0.855 0.088 16 0.0055CUGND116B D C1 4 1 11.498 17.331 0.849 0.088 16 0.0055CUGND117B D C1 4 1 11.252 17.079 0.859 0.088 16 0.0055CUGND118B D C1 4 1 10.991 17.017 0.831 0.089 16 0.0055CUGND215B D C2 4 2 10.848 17.384 0.837 0.089 16 0.0056CUGND216B D C2 4 2 11.396 17.393 0.852 0.088 16 0.0055CUGND217B D C2 4 2 10.912 17.276 0.841 0.090 16 0.0056CUGNE117B E C1 5 1 11.021 17.739 0.852 0.089 16 0.0056CUGNE118B E C1 5 1 11.256 17.648 0.852 0.089 16 0.0056CUGNE119B E C1 5 1 10.639 17.797 0.844 0.089 16 0.0056CUGNE11AB E C1 5 1 11.997 16.468 0.857 0.089 16 0.0056CUGNE216B E C2 5 2 12.321 17.556 0.865 0.088 16 0.0055CUGNE217B E C2 5 2 12.003 16.997 0.843 0.089 16 0.0056CUGNE218B E C2 5 2 10.972 18.252 0.864 0.088 16 0.0055CUGNF117B F C1 6 1 11.291 16.703 0.831 0.087 16 0.0054CUGNF118B F C1 6 1 11.177 16.456 0.832 0.088 16 0.0055CUGNF119B F C1 6 1 10.816 16.434 0.813 0.088 16 0.0055CUGNF11AB F C1 6 1 10.704 16.245 0.807 0.088 16 0.0055CUGNF216B F C2 6 2 11.163 17.360 0.800 0.089 16 0.0056CUGNF217B F C2 6 2 11.834 17.027 0.791 0.090 16 0.0056CUGNF218B F C2 6 2 11.169 17.523 0.829 0.089 16 0.0056

Strength at 5% strain is not available because strain gage failed prior to reaching 5% strain.

Average 11.269 17.198 0.838 Average 0.0055Standard Dev. 0.451 0.517 0.021 Standard Dev.

Coeff. of Var. [%] 3.999 3.004 2.505 Coeff. of Var. [%]Min. 10.639 16.245 0.791 Min. 0.0054Max. 12.321 18.252 0.865 Max. 0.0056

Number of Spec. 21 21 21 Number of Spec. 21

In-Plane Shear Properties (IPS)--CTDStrength & Modulus



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In‐Plane Shear Strength [ksi]

In-Plane Shear Properties (IPS)--CTDMeasured Strength at 0.2% Offset


Cure Cycle #

Prepreg Lot #

3

4

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6

7

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Cure Cycle #


In-Plane Shear Properties (IPS)--CTDMeasured Strength at Peak before 5% Strain


Cure Cycle #

Prepreg Lot #


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Cure Cycle #

In‐Plane Shear Modulus [Msi]

In-Plane Shear Properties (IPS)--CTDMeasured Modulus


Cure Cycle #

Prepreg Lot #


of 317

Specimen Number

Cytec Batch #

Cytec Cure Cycle

Prepreg Lot # Cure Cycle #0.2% Offset

Strength [ksi]

Strength at 5% Strain

[ksi]

Modulus [Msi]


[in]

# Plies in Laminate

Avg. tply [in]

CUGND111A D C1 4 1 8.316 13.644 0.751 0.086 16 0.0054CUGND112A D C1 4 1 8.015 13.420 0.715 0.087 16 0.0054CUGND113A D C1 4 1 8.111 13.591 0.721 0.088 16 0.0055CUGND114A D C1 4 1 8.072 13.411 0.715 0.089 16 0.0056CUGND211A D C2 4 2 8.015 13.363 0.719 0.088 16 0.0055CUGND213A D C2 4 2 8.199 13.640 0.720 0.088 16 0.0055CUGND214A D C2 4 2 7.820 13.055 0.707 0.088 16 0.0055CUGNE111A E C1 5 1 8.161 13.257 0.745 0.088 16 0.0055CUGNE112A E C1 5 1 8.144 13.475 0.726 0.089 16 0.0056CUGNE113A E C1 5 1 8.033 13.483 0.717 0.089 16 0.0055CUGNE114A E C1 5 1 8.038 13.462 0.711 0.089 16 0.0056CUGNE211A E C2 5 2 8.430 13.200 0.756 0.088 16 0.0055CUGNE212A E C2 5 2 8.090 13.552 0.720 0.088 16 0.0055CUGNE213A E C2 5 2 8.114 13.490 0.716 0.089 16 0.0056CUGNF111A F C1 6 1 8.212 13.696 0.702 0.087 16 0.0055CUGNF112A F C1 6 1 8.143 13.629 0.706 0.089 16 0.0055CUGNF113A F C1 6 1 8.153 13.693 0.703 0.087 16 0.0055CUGNF114A F C1 6 1 8.147 13.576 0.707 0.088 16 0.0055CUGNF211A F C2 6 2 8.120 13.548 0.720 0.087 16 0.0055CUGNF212A F C2 6 2 8.106 13.697 0.702 0.088 16 0.0055CUGNF213A F C2 6 2 8.093 13.648 0.704 0.089 16 0.0055




In-Plane Shear Properties (IPS)--RTDStrength & Modulus



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Strength [ksi]


[ksi]

Modulus [Msi]


[in]

# Plies in Laminate

Avg. tply [in]

CUGND119D D C1 4 1 5.211 8.297 0.557 0.088 16 0.0055CUGND11AD D C1 4 1 5.023 7.935 0.532 0.088 16 0.0055CUGND11BD D C1 4 1 5.283 8.234 0.564 0.089 16 0.0055CUGND11CD* D C1 4 1 5.132 0.545 0.087 16 0.0055CUGND219D D C2 4 2 5.166 8.238 0.548 0.089 16 0.0056CUGND21AD D C2 4 2 5.143 8.129 0.546 0.088 16 0.0055CUGND21BD D C2 4 2 5.096 8.159 0.540 0.090 16 0.0056*Strength at 5% strain is not available because strain gage failed prior to reaching 5% strain.




In-Plane Shear Properties (IPS)--ETW1Strength & Modulus



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Strength [ksi]


[ksi]

Modulus [Msi]


[in]

# Plies in Laminate

Avg. tply [in]

CUGND11EF D C1 4 1 2.913 5.026 0.303 0.089 16 0.0056CUGND11FF D C1 4 1 3.090 5.197 0.328 0.088 16 0.0055CUGND11GF D C1 4 1 3.215 5.402 0.347 0.088 16 0.0055CUGND11HF D C1 4 1 2.954 5.197 0.313 0.087 16 0.0054CUGND21EF D C2 4 2 3.219 5.388 0.348 0.089 16 0.0055CUGND21FF D C2 4 2 3.229 5.413 0.340 0.089 16 0.0056CUGND21GF* D C2 4 2 3.170 0.336 0.089 16 0.0056CUGNE11DF E C1 5 1 2.932 4.980 0.310 0.089 16 0.0056CUGNE11EF E C1 5 1 3.034 5.119 0.319 0.090 16 0.0056CUGNE11FF E C1 5 1 2.668 4.695 0.275 0.090 16 0.0056CUGNE11GF E C1 5 1 2.934 4.966 0.308 0.090 16 0.0056CUGNE21BF E C2 5 2 3.176 5.279 0.341 0.089 16 0.0055CUGNE21CF E C2 5 2 2.910 5.074 0.301 0.089 16 0.0056CUGNE21DF E C2 5 2 3.175 5.438 0.341 0.089 16 0.0055

CUGNF11DF** F C1 6 1 3.129 0.331 0.088 16 0.0055CUGNF11EF F C1 6 1 3.430 5.335 0.373 0.089 16 0.0055CUGNF11FF* F C1 6 1 3.181 0.337 0.088 16 0.0055CUGNF11GF F C1 6 1 3.145 5.238 0.342 0.088 16 0.0055CUGNF11HF F C1 6 1 2.948 5.003 0.316 0.089 16 0.0055CUGNF11IF F C1 6 1 2.939 4.946 0.313 0.088 16 0.0055CUGNF21BF F C2 6 2 3.107 5.116 0.329 0.089 16 0.0056CUGNF21CF F C2 6 2 2.816 4.926 0.299 0.089 16 0.0056CUGNF21DF F C2 6 2 3.058 5.037 0.317 0.089 16 0.0056

*Strength at 5% strain is not available because strain gage failed prior to reaching 5% strain.**Strength at 5% strain is not available due to the strain gauge malfunction during testing.




In-Plane Shear Properties (IPS)--ETW2Strength & Modulus



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[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGAD115B D C1 4 1 90.002 7.789 0.087 16 LGM 0.0055 89.423 7.739CUGAD116B D C1 4 1 91.891 7.585 0.089 16 LWT 0.0055 92.622 7.645CUGAD117B D C1 4 1 89.208 7.683 0.088 16 LGM 0.0055 89.647 7.721CUGAD118B D C1 4 1 91.921 7.657 0.088 16 LGM 0.0055 92.391 7.697CUGAD215B D C2 4 2 87.485 7.441 0.088 16 LWB 0.0055 87.187 7.416CUGAD216B D C2 4 2 87.194 7.503 0.088 16 LWB 0.0055 87.591 7.537CUGAD217B D C2 4 2 96.297 7.820 0.087 16 LGM 0.0055 95.477 7.753CUGAE117B E C1 5 1 90.755 7.754 0.089 16 LGM 0.0056 91.615 7.828CUGAE118B E C1 5 1 91.022 7.648 0.090 16 LGM 0.0056 93.159 7.828CUGAE119B E C1 5 1 92.080 7.674 0.089 16 LGM 0.0056 93.021 7.752CUGAE11AB E C1 5 1 90.519 7.643 0.089 16 LGM 0.0056 91.959 7.764CUGAE216B E C2 5 2 94.271 7.811 0.088 16 LWT 0.0055 94.253 7.810CUGAE217B E C2 5 2 91.733 7.887 0.088 16 LGM 0.0055 91.577 7.874CUGAE218B E C2 5 2 94.134 7.781 0.088 16 LGM 0.0055 94.348 7.799CUGAF117B F C1 6 1 87.524 7.663 0.088 16 LGM 0.0055 87.872 7.694CUGAF118B F C1 6 1 96.493 7.685 0.088 16 LGM 0.0055 96.950 7.721CUGAF119B F C1 6 1 89.629 7.634 0.089 16 LGM 0.0055 90.410 7.701CUGAF11AB F C1 6 1 95.810 7.651 0.088 16 LGM 0.0055 95.447 7.622CUGAF216B F C2 6 2 95.301 7.642 0.088 16 LGM 0.0055 94.832 7.605CUGAF217B F C2 6 2 96.632 7.624 0.088 16 LGM 0.0055 97.145 7.665CUGAF218B F C2 6 2 96.287 7.760 0.088 16 LGM 0.0055 95.849 7.725

Average 92.199 7.683 Averagenorm 0.0055 92.513 7.709Standard Dev. 3.150 0.105 Standard Dev.norm 3.004 0.105

Coeff. of Var. [%] 3.417 1.371 Coeff. of Var. [%]norm 3.247 1.368Min. 87.194 7.441 Min. 0.0055 87.187 7.416Max. 96.632 7.887 Max. 0.0056 97.145 7.874

Number of Spec. 21 21 Number of Spec. 21 21 21

Laminate Unnotched Tension Properties (UNT1)--CTDStrength & Modulus



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Laminate Unnotched Tension Properties (UNT1)--CTDNormalized Strength


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Laminate Unnotched Tension Properties (UNT1)--CTDNormalized Modulus


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[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGAD111A* D C1 4 1 98.353 7.609 0.087 16 LGM 0.0054 96.714 7.482CUGAD112A* D C1 4 1 94.456 7.598 0.088 16 LGM 0.0055 94.223 7.579CUGAD113A D C1 4 1 95.715 7.572 0.087 16 LGM 0.0055 95.134 7.526CUGAD114A D C1 4 1 92.616 7.374 0.088 16 LWT 0.0055 92.984 7.403CUGAD211A D C2 4 2 99.409 7.977 0.086 16 LGM 0.0054 97.150 7.796CUGAD212A D C2 4 2 98.359 7.619 0.087 16 AGM / LGM 0.0054 97.223 7.531CUGAD213A D C2 4 2 96.572 7.683 0.087 16 AGM 0.0054 95.383 7.588CUGAE111A E C1 5 1 94.098 7.599 0.090 16 LGM 0.0056 95.720 7.730CUGAE112A E C1 5 1 97.514 7.569 0.089 16 LWB 0.0056 98.512 7.646CUGAE113A E C1 5 1 98.682 7.727 0.089 16 LGM 0.0055 99.317 7.777CUGAE114A E C1 5 1 97.954 7.609 0.088 16 LGM 0.0055 98.009 7.613CUGAE211A E C2 5 2 95.001 7.850 0.086 16 LWB 0.0054 92.787 7.667CUGAE212A E C2 5 2 98.037 7.527 0.088 16 LWB 0.0055 98.278 7.546CUGAE213A E C2 5 2 100.852 7.807 0.089 16 LWB / LWT 0.0056 102.551 7.939CUGAF111A F C1 6 1 98.681 7.504 0.088 16 LAT 0.0055 98.644 7.501CUGAF112A F C1 6 1 98.986 7.475 0.089 16 LGM 0.0055 99.623 7.523CUGAF113A F C1 6 1 102.999 7.551 0.088 16 LGM 0.0055 102.902 7.544CUGAF114A F C1 6 1 98.648 7.386 0.089 16 LGM 0.0055 99.414 7.444CUGAF211A F C2 6 2 95.914 7.576 0.088 16 LGM 0.0055 95.369 7.533CUGAF212A F C2 6 2 103.154 7.427 0.087 16 LGM 0.0055 102.294 7.366CUGAF213A F C2 6 2 96.484 7.343 0.089 16 LWB 0.0056 97.818 7.445





Laminate Unnotched Tension Properties (UNT1)--RTDStrength & Modulus



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Laminate Unnotched Tension Properties (UNT1)--RTDNormalized Strength


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Laminate Unnotched Tension Properties (UNT1)--RTDNormalized Modulus


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[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGAD119D D C1 4 1 103.653 7.050 0.088 16 LAB / LWB / AWT 0.0055 103.810 7.061CUGAD11AD D C1 4 1 107.700 7.511 0.088 16 LWB / LGM 0.0055 107.109 7.469CUGAD11BD D C1 4 1 105.716 7.264 0.089 16 LWB / LWT 0.0055 106.417 7.312CUGAD11CD D C1 4 1 105.111 6.942 0.088 16 LGM / LWB 0.0055 104.792 6.921CUGAD219D D C2 4 2 106.010 6.999 0.087 16 LAB / AWT 0.0054 104.906 6.926CUGAD21AD D C2 4 2 113.558 7.627 0.087 16 LWB / AWT 0.0054 112.181 7.534CUGAD21BD D C2 4 2 97.548 7.271 0.088 16 LGM 0.0055 97.105 7.238




Laminate Unnotched Tension Properties (UNT1)--ETW1Strength & Modulus



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[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGAD11EF D C1 4 1 103.631 6.899 0.089 16 LGM 0.0055 104.279 6.942CUGAD11FF D C1 4 1 103.573 6.753 0.089 16 AGM / LGM 0.0055 104.299 6.800CUGAD11GF D C1 4 1 102.360 6.874 0.089 16 LGM / DGM 0.0056 103.368 6.942CUGAD11HF D C1 4 1 99.786 6.671 0.089 16 LGM / DGM 0.0055 100.618 6.727CUGAD21EF D C2 4 2 99.870 6.796 0.087 16 LGM / DGM 0.0054 98.830 6.725CUGAD21FF D C2 4 2 100.975 6.704 0.088 16 LWT / LWB 0.0055 101.358 6.730CUGAD21GF D C2 4 2 101.830 6.955 0.088 16 LGM / DGM 0.0055 101.540 6.936CUGAE11DF E C1 5 1 102.150 7.196 0.089 16 LWB / LWT / DGM 0.0056 103.136 7.266CUGAE11EF E C1 5 1 104.272 6.872 0.090 16 LGM / AGM 0.0056 106.149 6.996CUGAE11FF E C1 5 1 101.840 7.141 0.089 16 AGM 0.0056 103.402 7.251CUGAE11GF E C1 5 1 104.025 6.786 0.089 16 DGM / LGM 0.0055 104.695 6.830CUGAE21BF E C2 5 2 110.454 7.307 0.089 16 LGM / LWB 0.0056 111.772 7.395CUGAE21CF E C2 5 2 105.487 7.458 0.088 16 LGM 0.0055 105.847 7.483CUGAE21DF E C2 5 2 94.640 7.077 0.089 16 LWT 0.0056 96.092 7.185CUGAF11DF F C1 6 1 100.626 6.779 0.089 16 LGM 0.0056 102.093 6.878CUGAF11EF F C1 6 1 102.338 6.850 0.089 16 AWT / LWT / DGM 0.0055 103.016 6.895CUGAF11FF F C1 6 1 99.373 6.615 0.089 16 AGM 0.0056 100.596 6.696CUGAF11GF F C1 6 1 101.978 6.923 0.088 16 AGM 0.0055 102.441 6.954CUGAF21BF F C2 6 2 106.632 6.920 0.088 16 LGM 0.0055 106.248 6.896CUGAF21CF F C2 6 2 105.115 6.718 0.088 16 LGM 0.0055 104.975 6.709CUGAF21DF F C2 6 2 104.891 6.949 0.089 16 LGM 0.0055 105.626 6.997







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[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGBD117B D C1 4 1 67.536 5.128 0.109 20 AWT 0.0055 67.044 5.091CUGBD118B D C1 4 1 67.378 5.131 0.111 20 AGM 0.0055 67.776 5.162CUGBD119B D C1 4 1 71.068 5.222 0.109 20 AGM 0.0055 70.443 5.176CUGBD11AB D C1 4 1 70.754 5.089 0.110 20 AWT 0.0055 70.733 5.087CUGBD216B D C2 4 2 68.698 4.989 0.110 20 AWB 0.0055 68.469 4.973CUGBD217B D C2 4 2 71.623 5.077 0.110 20 AWB 0.0055 71.645 5.079CUGBD218B D C2 4 2 69.340 5.159 0.110 20 AWB 0.0055 69.350 5.159CUGBE117B E C1 5 1 70.772 5.195 0.110 20 AWB 0.0055 70.740 5.193CUGBE118B E C1 5 1 70.382 5.232 0.110 20 AWB 0.0055 70.649 5.252CUGBE119B E C1 5 1 66.653 5.136 0.111 20 AGM 0.0056 67.481 5.200CUGBE11AB E C1 5 1 70.164 5.215 0.110 20 AWB 0.0055 70.419 5.234CUGBE216B E C2 5 2 69.779 5.109 0.111 20 AWT 0.0056 70.445 5.158CUGBE217B E C2 5 2 69.516 5.147 0.111 20 AWT 0.0056 70.179 5.196CUGBE218B E C2 5 2 72.163 5.082 0.111 20 AWT 0.0056 73.093 5.148CUGBF114B F C1 6 1 72.180 5.016 0.112 20 AWB 0.0056 73.569 5.113CUGBF115B F C1 6 1 74.238 4.897 0.113 20 AGM 0.0056 75.970 5.011CUGBF116B F C1 6 1 73.243 5.021 0.112 20 AWB 0.0056 74.297 5.094CUGBF217B F C2 6 2 75.468 4.992 0.111 20 AGM 0.0056 76.326 5.049CUGBF218B F C2 6 2 72.663 4.974 0.112 20 AWB 0.0056 73.963 5.063CUGBF219B F C2 6 2 73.227 5.018 0.111 20 AGM 0.0056 73.893 5.063CUGBF21AB F C2 6 2 69.856 5.041 0.112 20 AWB 0.0056 70.862 5.113




Laminate Unnotched Tension Properties (UNT2) --CTDStrength & Modulus



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[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGBD111A* D C1 4 1 67.305 4.835 0.109 20 AGM 0.0054 66.398 4.770CUGBD112A* D C1 4 1 69.012 4.978 0.108 20 AGM 0.0054 67.548 4.873CUGBD113A D C1 4 1 69.071 4.949 0.109 20 AGM 0.0054 68.224 4.888CUGBD114A D C1 4 1 69.589 4.868 0.110 20 AGM 0.0055 69.504 4.862CUGBD211A D C2 4 2 65.124 4.971 0.109 20 AGM 0.0054 64.502 4.923CUGBD212A D C2 4 2 68.186 4.916 0.110 20 AGM 0.0055 68.114 4.911CUGBD213A D C2 4 2 65.250 4.951 0.109 20 AWT 0.0055 64.805 4.917CUGBE111A E C1 5 1 70.976 5.065 0.109 20 AGM 0.0055 70.643 5.042CUGBE112A E C1 5 1 68.836 4.936 0.111 20 AGM 0.0055 69.451 4.980CUGBE113A E C1 5 1 69.436 4.810 0.111 20 AGM 0.0056 70.109 4.857CUGBE114A E C1 5 1 66.438 4.953 0.111 20 AWT 0.0055 66.951 4.991CUGBE211A E C2 5 2 65.034 5.005 0.110 20 AGM 0.0055 64.876 4.993CUGBE212A E C2 5 2 69.805 4.977 0.110 20 AGM 0.0055 69.679 4.968CUGBE213A E C2 5 2 68.522 5.201 0.110 20 AWB 0.0055 68.449 5.196CUGBF111A F C1 6 1 66.834 4.884 0.111 20 AWB / DGM 0.0055 67.422 4.927CUGBF112A F C1 6 1 66.670 4.899 0.112 20 AWT 0.0056 67.731 4.977CUGBF113A F C1 6 1 68.919 4.723 0.111 20 DGM / AWB 0.0056 69.828 4.785CUGBF211A F C2 6 2 68.338 4.870 0.109 20 DGM / AWT 0.0055 67.717 4.825CUGBF212A F C2 6 2 64.807 4.901 0.111 20 AWT 0.0056 65.612 4.962CUGBF213A F C2 6 2 63.838 4.741 0.112 20 AWB 0.0056 64.824 4.815CUGBF214A F C2 6 2 67.208 4.751 0.111 20 DGM / AGM 0.0056 67.900 4.800





Laminate Unnotched Tension Properties (UNT2) --RTDStrength & Modulus



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[Msi]


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# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGBD11DF D C1 4 1 52.084 4.188 0.109 20 DGM / AGM 0.0055 51.761 4.162CUGBD11EF D C1 4 1 50.405 4.146 0.109 20 DGM / AGM 0.0055 50.092 4.120CUGBD11FF D C1 4 1 51.053 4.314 0.109 20 DGM / AGM 0.0054 50.504 4.268CUGBD11GF D C1 4 1 50.658 4.311 0.110 20 DGM / AGM 0.0055 50.666 4.312CUGBD21BF D C2 4 2 49.793 4.076 0.112 20 DGM / AGM 0.0056 50.600 4.142CUGBD21CF D C2 4 2 49.837 4.187 0.111 20 DGM / AGM 0.0055 50.132 4.211CUGBD21DF D C2 4 2 49.349 4.071 0.110 20 DGM / AGM 0.0055 49.200 4.059CUGBE11DF E C1 5 1 50.046 3.991 0.112 20 DGM / AGM 0.0056 50.797 4.051CUGBE11EF E C1 5 1 50.076 4.106 0.112 20 DGM / AGM 0.0056 50.759 4.162CUGBE11FF E C1 5 1 50.137 4.022 0.112 20 DGM / AGM 0.0056 50.821 4.076CUGBE11GF E C1 5 1 50.490 3.992 0.111 20 DGM / AGM 0.0055 50.734 4.012CUGBE21BF E C2 5 2 51.426 4.314 0.110 20 DGM / AGM 0.0055 51.472 4.318CUGBE21CF E C2 5 2 50.498 4.119 0.111 20 DGM / AGM 0.0056 50.987 4.158CUGBE21EF E C2 5 2 50.080 4.087 0.111 20 DGM / AGM 0.0055 50.376 4.111CUGBF117F F C1 6 1 49.461 4.175 0.112 20 DGM / AGM 0.0056 50.136 4.232CUGBF118F F C1 6 1 49.878 4.029 0.112 20 DGM / AGM 0.0056 50.740 4.099CUGBF119F F C1 6 1 47.045 4.141 0.111 20 DGM / AGM 0.0056 47.580 4.188CUGBF21DF F C2 6 2 47.994 4.133 0.111 20 DGM / AGM 0.0056 48.612 4.186CUGBF21EF F C2 6 2 47.768 4.340 0.112 20 DGM / AGM 0.0056 48.441 4.401CUGBF21FF F C2 6 2 48.330 4.125 0.111 20 DGM / AGM 0.0056 48.858 4.170CUGBF21GF F C2 6 2 49.015 4.157 0.111 20 DGM / AGM 0.0055 49.453 4.195




Laminate Unnotched Tension Properties (UNT2) --ETW2Strength & Modulus



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Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGCD117B D C1 4 1 145.860 11.516 0.109 20 LAT 0.0055 144.910 11.440CUGCD118B D C1 4 1 142.082 11.854 0.110 20 LAT 0.0055 141.630 11.816CUGCD119B D C1 4 1 133.604 11.825 0.110 20 LAT 0.0055 133.118 11.782CUGCD11AB D C1 4 1 143.788 12.212 0.109 20 LWT / LAB 0.0054 141.936 12.054CUGCD216B D C2 4 2 137.425 11.799 0.110 20 LAB 0.0055 137.258 11.785CUGCD217B D C2 4 2 135.810 11.950 0.108 20 LAT 0.0054 133.875 11.779CUGCD218B D C2 4 2 136.125 11.710 0.109 20 LAT 0.0055 135.176 11.628CUGCE117B E C1 5 1 139.319 11.813 0.111 20 LAB 0.0056 140.860 11.944CUGCE118B E C1 5 1 146.961 11.785 0.111 20 LAT 0.0055 147.852 11.856CUGCE119B E C1 5 1 139.446 11.778 0.111 20 LAT 0.0056 141.242 11.929CUGCE11AB E C1 5 1 148.353 11.778 0.110 20 LWT / LAB 0.0055 148.781 11.812CUGCE216B E C2 5 2 148.785 12.071 0.109 20 LAB 0.0055 147.568 11.973CUGCE217B E C2 5 2 142.476 11.836 0.111 20 LAB 0.0055 143.361 11.910CUGCE218B E C2 5 2 143.171 11.829 0.109 20 LAB 0.0055 142.412 11.766CUGCF117B F C1 6 1 146.165 11.381 0.112 20 LAB 0.0056 148.756 11.583CUGCF118B F C1 6 1 145.882 11.420 0.112 20 LAB 0.0056 148.424 11.619CUGCF119B F C1 6 1 144.050 11.738 0.112 20 LAB 0.0056 147.062 11.983CUGCF11AB F C1 6 1 153.303 11.606 0.112 20 LAB 0.0056 156.044 11.814CUGCF216B F C2 6 2 141.114 11.485 0.112 20 LWB / AWB 0.0056 143.145 11.650CUGCF217B F C2 6 2 145.020 11.676 0.112 20 LWB 0.0056 147.349 11.863CUGCF218B F C2 6 2 157.692 11.687 0.112 20 LAB 0.0056 160.869 11.923




Laminate Unnotched Tension Properties (UNT3)--CTDStrength & Modulus



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Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGCD111A* D C1 4 1 151.209 11.807 0.107 20 LAB 0.0053 146.718 11.457CUGCD112A* D C1 4 1 161.850 11.671 0.110 20 AWT / AWB 0.0055 162.487 11.717CUGCD113A D C1 4 1 164.324 11.864 0.110 20 LAT / LWB 0.0055 164.822 11.900CUGCD114A D C1 4 1 144.562 11.502 0.109 20 LAT 0.0055 143.488 11.417CUGCD211A D C2 4 2 150.226 11.580 0.110 20 LAT / LAB 0.0055 150.203 11.578CUGCD212A D C2 4 2 157.693 11.562 0.109 20 LAB 0.0055 156.761 11.493CUGCD213A D C2 4 2 140.471 11.729 0.110 20 LAT 0.0055 140.003 11.690CUGCE111A E C1 5 1 157.874 11.813 0.110 20 AAB / LWT 0.0055 157.228 11.765CUGCE112A E C1 5 1 150.474 11.851 0.110 20 LAT 0.0055 150.702 11.869CUGCE113A E C1 5 1 150.757 11.716 0.111 20 LAT 0.0056 152.424 11.845CUGCE114A E C1 5 1 149.767 11.760 0.111 20 LAT 0.0056 151.786 11.919CUGCE211A E C2 5 2 152.132 11.610 0.109 20 LAT 0.0055 151.117 11.532CUGCE212A E C2 5 2 152.770 11.693 0.109 20 LAT 0.0054 150.802 11.542CUGCE213A E C2 5 2 157.479 12.266 0.111 20 LAT / LWB 0.0055 158.457 12.342CUGCF111A F C1 6 1 144.058 11.413 0.111 20 LAB 0.0056 145.760 11.548CUGCF112A F C1 6 1 140.268 11.398 0.112 20 LAT 0.0056 142.435 11.574CUGCF113A F C1 6 1 159.981 11.430 0.113 20 LAB / LWT 0.0056 164.174 11.729CUGCF114A F C1 6 1 158.764 11.425 0.112 20 LAB / LAT / AWT 0.0056 162.011 11.658CUGCF211A F C2 6 2 162.846 11.596 0.112 20 LAB / AWT 0.0056 165.067 11.754CUGCF212A F C2 6 2 143.005 11.452 0.112 20 LAB 0.0056 145.172 11.625CUGCF213A F C2 6 2 ** 11.461 0.112 20 LIT 0.0056 11.630CUGCF214A F C2 6 2 155.198 11.511 0.112 20 LAB 0.0056 158.632 11.766

* Strain measurement was measured with SG. Extensometer used on other coupons. ** Strength not reported due to unacceptable failure mode.




Laminate Unnotched Tension Properties (UNT3)--RTDStrength & Modulus



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Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGCD11DF D C1 4 1 * 11.477 0.109 20 LIT 0.0054 11.357CUGCD11EF D C1 4 1 * 11.802 0.108 20 LIT 0.0054 11.543CUGCD11FF D C1 4 1 166.536 11.181 0.109 20 AWT / LWB 0.0055 165.073 11.083CUGCD11GF D C1 4 1 164.658 11.781 0.109 20 DGM / LGM / LAB 0.0055 163.560 11.702CUGCD11HF D C1 4 1 167.465 11.612 0.109 20 LWT/ LAB 0.0054 165.334 11.464CUGCD11IF D C1 4 1 164.160 11.859 0.109 20 LAB 0.0055 162.742 11.756CUGCD21BF D C2 4 2 166.684 11.342 0.110 20 AWT / LWB 0.0055 166.684 11.342CUGCD21CF D C2 4 2 174.740 11.735 0.110 20 AWB / LWT 0.0055 174.766 11.737CUGCD21DF D C2 4 2 170.136 11.238 0.110 20 LAT / LWB 0.0055 169.955 11.226CUGCE11DF E C1 5 1 160.137 11.479 0.111 20 LWT / AWB 0.0056 162.030 11.614CUGCE11EF E C1 5 1 165.033 11.509 0.112 20 LWT / LAB 0.0056 167.484 11.680CUGCE11FF E C1 5 1 162.866 11.663 0.112 20 LWT / LWB 0.0056 165.458 11.849CUGCE11GF E C1 5 1 151.999 11.318 0.112 20 LWT / LAB 0.0056 154.671 11.517CUGCE21BF E C2 5 2 174.438 11.663 0.111 20 AWT 0.0056 176.367 11.792CUGCE21CF E C2 5 2 170.940 11.478 0.111 20 AWT / LWB 0.0056 172.986 11.615CUGCE21DF E C2 5 2 169.816 11.537 0.112 20 AWT 0.0056 173.238 11.770CUGCF11DF F C1 6 1 150.687 11.231 0.113 20 LIB / LWT 0.0056 154.134 11.488CUGCF11EF F C1 6 1 157.608 11.453 0.112 20 AWT 0.0056 160.425 11.658CUGCF11FF F C1 6 1 148.996 11.300 0.113 20 LWT / AWB 0.0056 152.789 11.587CUGCF11GF F C1 6 1 162.575 11.184 0.112 20 LWT / AWB 0.0056 165.876 11.411CUGCF21BF F C2 6 2 155.134 11.636 0.112 20 LWT / LWB 0.0056 157.673 11.826CUGCF21CF F C2 6 2 164.075 11.430 0.112 20 DGM / AGM 0.0056 167.655 11.679CUGCF21DF F C2 6 2 161.711 11.335 0.112 20 AGM / LAB 0.0056 163.990 11.495

*Strength not reported due to unacceptable failure mode.







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Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGRD117B D C1 4 1 100.846 6.753 0.112 21 BGM 0.0053 97.452 6.526CUGRD118B D C1 4 1 99.312 7.182 0.113 21 BGM 0.0054 96.743 6.996CUGRD119B D C1 4 1 109.729 7.180 0.113 21 BGM 0.0054 107.057 7.005CUGRD11AB D C1 4 1 * 7.052 0.112 21 HIB 0.0053 6.827CUGRD216B D C2 4 2 101.316 6.999 0.115 21 BGM 0.0055 101.086 6.983CUGRD217B D C2 4 2 95.335 6.841 0.116 21 BGM 0.0055 95.706 6.867CUGRD218B D C2 4 2 94.710 7.004 0.116 21 BGM 0.0055 94.803 7.011CUGRE117B E C1 5 1 113.808 6.938 0.114 21 BGM 0.0054 112.552 6.861CUGRE118B E C1 5 1 98.509 7.101 0.115 21 BGM 0.0055 97.997 7.064CUGRE119B E C1 5 1 113.067 7.157 0.116 21 BGM 0.0055 113.079 7.158CUGRE11AB E C1 5 1 * 7.304 0.115 21 HIB 0.0055 7.284CUGRE11BB E C1 5 1 100.967 ** 0.115 21 BGM 0.0055 100.956CUGRE216B E C2 5 2 94.098 7.035 0.115 21 BGM 0.0055 93.457 6.987CUGRE217B E C2 5 2 94.460 6.833 0.115 21 BGM 0.0055 93.785 6.784CUGRE218B E C2 5 2 * 7.027 0.114 21 HIT / BGM 0.0054 6.957CUGRE21AB E C2 5 2 94.216 ** 0.115 21 BGM 0.0055 93.472CUGRF117B F C1 6 1 106.656 6.559 0.115 21 BGM 0.0055 106.009 6.519CUGRF118B F C1 6 1 91.206 6.019 0.115 21 BGM 0.0055 91.019 6.007CUGRF119B F C1 6 1 84.042 6.472 0.114 21 BGM 0.0054 82.923 6.386CUGRF11AB F C1 6 1 92.680 6.258 0.115 21 BGM 0.0055 91.968 6.210CUGRF11BB F C1 6 1 97.183 ** 0.114 21 BGM 0.0054 96.279CUGRF216B F C2 6 2 92.382 5.968 0.116 21 BGM 0.0055 92.702 5.989CUGRF217B F C2 6 2 99.971 6.307 0.116 21 BGM 0.0055 100.253 6.324CUGRF218B F C2 6 2 90.948 6.070 0.116 21 BGM 0.0055 91.509 6.107

*Strength not reported due to unacceptable failure mode.**Specimen was not gaged.




Laminate Unnotched Compression Properties (UNC0)--CTDStrength & Modulus



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Laminate Unnotched Compression Strength [ksi]

Laminate Unnotched Compression Properties (UNC0)--CTDNormalized Strength


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Laminate Unnotched Compression Modulus [Msi]

Laminate Unnotched Compression Properties (UNC0)--CTDNormalized Modulus


Cure Cycle #

Prepreg Lot #


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Specimen Number

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Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGRD112A D C1 4 1 * 7.028 0.112 21 CIB/ HIB 0.0054 6.843CUGRD113A D C1 4 1 96.028 6.996 0.112 21 BGM 0.0053 93.305 6.798CUGRD114A D C1 4 1 92.928 6.863 0.113 21 BGM 0.0054 91.309 6.744CUGRD115A D C1 4 1 105.098 7.203 0.112 21 BGM 0.0053 101.879 6.983CUGRD116A D C1 4 1 87.563 ** 0.113 21 BGM 0.0054 85.317CUGRD212A D C2 4 2 95.663 7.502 0.116 21 BGM 0.0055 96.429 7.562CUGRD213A D C2 4 2 99.557 7.161 0.116 21 BGM 0.0055 100.311 7.216CUGRD214A D C2 4 2 85.606 6.983 0.118 21 BGM 0.0056 87.236 7.116CUGRE111A E C1 5 1 90.088 7.135 0.115 21 BGM 0.0055 89.327 7.075CUGRE112A E C1 5 1 94.330 7.164 0.116 21 BGM 0.0055 94.932 7.210CUGRE113A E C1 5 1 86.267 7.231 0.116 21 BGM 0.0055 86.716 7.269CUGRE114A E C1 5 1 87.969 7.243 0.115 21 BGM 0.0055 87.560 7.209CUGRE211A E C2 5 2 95.585 7.268 0.112 21 BGM 0.0053 92.647 7.045CUGRE212A E C2 5 2 95.320 7.282 0.115 21 BGM 0.0055 95.134 7.268CUGRE213A E C2 5 2 94.970 7.265 0.114 21 BGM 0.0054 94.004 7.191CUGRF111A F C1 6 1 82.226 7.088 0.115 21 BGM 0.0055 81.603 7.034CUGRF112A F C1 6 1 100.169 7.120 0.115 21 BGM 0.0055 99.757 7.091CUGRF113A F C1 6 1 91.606 7.018 0.114 21 BGM 0.0055 90.793 6.956CUGRF114A F C1 6 1 89.347 7.143 0.115 21 BGM 0.0055 88.950 7.112CUGRF212A F C2 6 2 89.871 6.843 0.115 21 BGM 0.0055 89.686 6.829CUGRF213A F C2 6 2 89.742 7.220 0.115 21 BGM 0.0055 89.655 7.213CUGRF214A F C2 6 2 92.784 7.159 0.116 21 BGM 0.0055 93.175 7.190





Laminate Unnotched Compression Properties (UNC0)--RTDStrength & Modulus



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Laminate Unnotched Compression Properties (UNC0)--RTDNormalized Strength


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Laminate Unnotched Compression Properties (UNC0)--RTDNormalized Modulus


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Prepreg Lot #


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Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGRD11DC D C1 4 1 89.424 7.299 0.112 21 BGM / HIT 0.0054 87.024 7.103CUGRD11EC D C1 4 1 89.660 7.019 0.115 21 BGM 0.0055 88.893 6.959CUGRD11FC D C1 4 1 82.487 7.012 0.114 21 BGM 0.0054 81.344 6.915CUGRD11GC D C1 4 1 83.197 7.150 0.116 21 BGM 0.0055 83.620 7.186CUGRD11HC D C1 4 1 90.111 * 0.116 21 BGM 0.0055 90.716CUGRD11IC D C1 4 1 80.801 * 0.115 21 BGM 0.0055 80.661CUGRD21BC D C2 4 2 83.983 6.838 0.117 21 HIT / BGM 0.0056 85.065 6.926CUGRD21CC D C2 4 2 87.585 6.782 0.117 21 HIT / BGM 0.0056 88.552 6.856CUGRD21DC D C2 4 2 89.305 6.809 0.116 21 CIT / HIB / BGM 0.0055 90.040 6.865CUGRD21EC D C2 4 2 87.774 * 0.117 21 HIT / BGM 0.0056 89.228CUGRD21FC D C2 4 2 85.868 * 0.116 21 BGM 0.0055 86.602*Specimen was not gaged.




Laminate Unnotched Compression Properties (UNC0)--ETD1Strength & Modulus



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Laminate Unnotched Compression Properties (UNC0)--ETD1Normalized Strength


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Laminate Unnotched Compression Properties (UNC0)--ETD1Normalized Modulus


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Specimen Number

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Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGRD131D D C1 4 1 7.018 0.111 21 BGM 0.0053 6.742CUGRD132D D C1 4 1 7.137 0.114 21 BGM 0.0054 7.055CUGRD133D D C1 4 1 6.909 0.115 21 BGM 0.0055 6.887CUGRD134D D C1 4 1 7.148 0.115 21 BGM 0.0055 7.131CUGRD135D D C1 4 1 78.414 0.115 21 BGM / HIB 0.0055 77.904CUGRD136D D C1 4 1 74.868 0.116 21 BGM / HIB 0.0055 75.070CUGRD137D D C1 4 1 75.991 0.115 21 HIB / BGM 0.0055 75.596CUGRD138D D C1 4 1 74.899 0.115 21 HIB / BGM 0.0055 74.713CUGRD232D D C2 4 2 7.478 0.115 21 BGM / HIT 0.0055 7.467CUGRD233D D C2 4 2 6.929 0.115 21 HIB / BGM 0.0055 6.892CUGRD234D D C2 4 2 7.387 0.115 21 HIB / BGM 0.0055 7.347CUGRD235D D C2 4 2 72.495 0.115 21 BGM 0.0055 71.961CUGRD236D D C2 4 2 77.071 0.114 21 BGM 0.0054 76.345CUGRD237D D C2 4 2 78.453 0.114 21 BGM 0.0054 77.400




Laminate Unnotched Compression Properties (UNC0)--ETW1Strength & Modulus



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Laminate Unnotched Compression Properties (UNC0)--ETW1Normalized Strength


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Laminate Unnotched Compression Properties (UNC0)--ETW1Normalized Modulus


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Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGRD11JE D C1 4 1 78.574 7.007 0.115 21 BGM 0.0055 78.209 6.974CUGRD11KE D C1 4 1 84.441 6.963 0.116 21 BGM 0.0055 84.478 6.966CUGRD11LE D C1 4 1 80.047 7.045 0.116 21 BGM/CIT 0.0055 80.723 7.104CUGRD11ME D C1 4 1 88.500 7.054 0.116 21 HGM/CIT 0.0055 88.500 7.054CUGRD21GE D C2 4 2 81.745 6.982 0.117 21 HGM 0.0056 82.524 7.048CUGRD21HE D C2 4 2 87.778 7.005 0.117 21 BGM / HIT 0.0056 88.605 7.071CUGRD21IE D C2 4 2 82.493 6.668 0.116 21 BGM 0.0055 82.734 6.687




Laminate Unnotched Compression Properties (UNC0)--ETD2Strength & Modulus



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Laminate Unnotched Compression Properties (UNC0)--ETD2Normalized Strength


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Laminate Unnotched Compression Properties (UNC0)--ETD2Normalized Modulus


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Specimen Number

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Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGRD13DF D C1 4 1 7.525 0.109 21 BGM / HIB 0.0052 7.086CUGRD13EF D C1 4 1 7.159 0.112 21 HIT 0.0053 6.952CUGRD13FF D C1 4 1 7.220 0.114 21 BGM 0.0054 7.097CUGRD13GF D C1 4 1 7.226 0.114 21 BGM / HIB 0.0054 7.123CUGRD13HF D C1 4 1 70.653 0.114 21 HIB / BGM 0.0054 69.690CUGRD13IF D C1 4 1 67.142 0.114 21 HIB / HGM 0.0054 66.503CUGRD13KF D C1 4 1 71.193 0.114 21 HIB / BGM 0.0054 69.999CUGRD13LF D C1 4 1 62.350 0.114 21 HIB / BGM 0.0054 61.513CUGRD23BF D C2 4 2 7.468 0.115 21 HIT / HIB / BGM 0.0055 7.468CUGRD23CF D C2 4 2 6.920 0.114 21 HIB / BGM 0.0054 6.855CUGRD23DF D C2 4 2 6.764 0.115 21 HIT / BGM 0.0055 6.734CUGRD23EF D C2 4 2 67.894 0.115 21 BGM / HIB 0.0055 67.827CUGRD23FF D C2 4 2 66.693 0.116 21 BGM / HIB 0.0055 66.714CUGRD23GF D C2 4 2 66.631 0.115 21 BGM / HAB 0.0055 66.321CUGRE11DF E C1 5 1 6.694 0.114 21 HIT / BGM 0.0054 6.632CUGRE11EF E C1 5 1 6.952 0.116 21 HAT / BGM 0.0055 6.952CUGRE11FF E C1 5 1 6.752 0.116 21 HIB / BGM 0.0055 6.754CUGRE11GF E C1 5 1 6.861 0.115 21 HIB / BGM 0.0055 6.822CUGRE11HF E C1 5 1 68.040 0.116 21 HIT / BGM 0.0055 68.194CUGRE11IF E C1 5 1 75.377 0.115 21 HIT / HIB / BGM 0.0055 74.912CUGRE11JF E C1 5 1 70.739 0.115 21 BGM / HIB 0.0055 70.371CUGRE11KF E C1 5 1 65.352 0.115 21 BGM 0.0055 65.175CUGRE21BF E C2 5 2 6.968 0.112 21 BGM 0.0053 6.736CUGRE21CF E C2 5 2 7.132 0.114 21 HIB / BGM 0.0054 7.057CUGRE21DF E C2 5 2 7.134 0.115 21 BGM / HIB 0.0055 7.084CUGRE21EF E C2 5 2 58.062 0.116 21 BGM 0.0055 58.125CUGRE21FF E C2 5 2 71.803 0.115 21 BGM / HIB 0.0055 71.779CUGRE21GF E C2 5 2 67.700 0.116 21 HAB / BGM 0.0055 67.744CUGRE21HF E C2 5 2 65.214 0.116 21 HAB / BGM 0.0055 65.426CUGRF11DF F C1 6 1 6.557 0.114 21 HGM 0.0054 6.481CUGRF11EF F C1 6 1 6.956 0.114 21 BGM / HIB 0.0054 6.872CUGRF11FF F C1 6 1 6.647 0.114 21 HIB / BGM 0.0054 6.581CUGRF11GF F C1 6 1 6.529 0.114 21 HIB / BAT 0.0054 6.442CUGRF11HF F C1 6 1 69.593 0.115 21 HGM 0.0055 69.066CUGRF11IF F C1 6 1 68.122 0.115 21 HIB / BGM 0.0055 67.953CUGRF11JF F C1 6 1 67.782 0.115 21 HGM / HIB 0.0055 67.218CUGRF21BF F C2 6 2 6.947 0.115 21 BGM 0.0055 6.900CUGRF21CF F C2 6 2 6.679 0.115 21 BGM / HIB 0.0055 6.673CUGRF21DF F C2 6 2 6.646 0.116 21 HAT / BGM 0.0055 6.646CUGRF21EF F C2 6 2 69.135 0.116 21 BGM / HAB 0.0055 69.427CUGRF21FF F C2 6 2 67.421 0.117 21 HIB / BGM 0.0056 68.129CUGRF21GF F C2 6 2 60.211 0.116 21 BGM 0.0055 60.681







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Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGWD111A D C1 4 1 93.712 7.515 0.127 24 BGM 0.0053 89.922 7.211CUGWD112A D C1 4 1 * 7.040 0.131 24 HIB 0.0055 7.006CUGWD113A D C1 4 1 95.031 7.122 0.129 24 BGM 0.0054 93.132 6.980CUGWD114A D C1 4 1 97.776 7.190 0.131 24 BGM 0.0055 96.905 7.126CUGWD115A D C1 4 1 91.303 ** 0.130 24 BGM 0.0054 90.076CUGWD211A D C2 4 2 97.314 7.753 0.125 24 HGM 0.0052 92.467 7.367CUGWD212A D C2 4 2 99.813 7.217 0.132 24 BGM 0.0055 99.690 7.208CUGWD213A D C2 4 2 105.790 7.313 0.131 24 HGM 0.0054 104.718 7.239CUGWE111A E C1 5 1 105.132 7.414 0.130 24 BGM 0.0054 103.310 7.286CUGWE112A E C1 5 1 106.483 7.433 0.132 24 BGM 0.0055 106.271 7.418CUGWE113A E C1 5 1 109.295 7.444 0.131 24 BGM 0.0055 108.860 7.414CUGWE114A E C1 5 1 101.815 7.370 0.132 24 BGM 0.0055 101.545 7.351CUGWE211A E C2 5 2 93.428 7.315 0.128 24 BGM 0.0053 90.845 7.113CUGWE212A E C2 5 2 100.814 7.253 0.130 24 BGM 0.0054 99.076 7.128CUGWE213A E C2 5 2 97.152 7.366 0.131 24 BGM 0.0054 96.121 7.288CUGWF111A F C1 6 1 93.723 7.420 0.125 24 BGM 0.0052 88.788 7.029CUGWF112A F C1 6 1 100.410 7.031 0.132 24 BGM 0.0055 100.134 7.012CUGWF113A F C1 6 1 102.599 7.095 0.133 24 BGM 0.0055 103.230 7.138CUGWF114A F C1 6 1 100.966 6.870 0.134 24 BGM 0.0056 102.582 6.980CUGWF211A F C2 6 2 84.338 7.750 0.122 24 BGM 0.0051 78.165 7.183CUGWF212A F C2 6 2 99.302 7.090 0.133 24 BGM 0.0055 99.791 7.125CUGWF213A F C2 6 2 87.104 7.322 0.133 24 BGM 0.0055 87.550 7.359CUGWF214A F C2 6 2 91.645 ** 0.133 24 BGM 0.0056 92.643*Strength not reported due to unacceptable failure mode.**Specimen was not gaged.







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Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGWE117D E C1 5 1 7.142 0.133 24 BGM 0.0055 7.192CUGWE118D E C1 5 1 7.371 0.132 24 BGM 0.0055 7.386CUGWE119D E C1 5 1 7.207 0.132 24 HIT/CIT/CIB 0.0055 7.213CUGWE11AD E C1 5 1 7.072 0.131 24 BGM / HIT/CIT 0.0055 7.044CUGWE11BD E C1 5 1 81.898 0.132 24 BGM 0.0055 81.859CUGWE11CD E C1 5 1 84.023 0.133 24 BGM 0.0055 84.366CUGWE11DD E C1 5 1 80.040 0.131 24 BGM 0.0055 79.615CUGWE11ED E C1 5 1 83.710 0.132 24 BGM / CIT 0.0055 83.940CUGWE11FD E C1 5 1 83.493 0.132 24 BGM 0.0055 83.319CUGWE11GD E C1 5 1 76.963 0.131 24 BGM 0.0055 76.344CUGWE217D E C2 5 2 7.132 0.132 24 BGM / CIT / CIB 0.0055 7.107CUGWE218D E C2 5 2 7.131 0.131 24 CIT / BGM 0.0055 7.090CUGWE219D E C2 5 2 7.142 0.133 24 CIT / HIB / BGM 0.0055 7.173CUGWE21BD E C2 5 2 83.741 0.132 24 BGM 0.0055 83.424CUGWE21CD E C2 5 2 84.828 0.132 24 BGM / HIB 0.0055 84.627CUGWE21ED E C2 5 2 78.989 0.130 24 BGM 0.0054 77.591







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Specimen Number

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Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGWD117F D C1 4 1 7.032 0.129 24 BGM 0.0054 6.896CUGWD118F D C1 4 1 6.766 0.129 24 BGM 0.0054 6.636CUGWD119F D C1 4 1 6.956 0.129 24 BGM 0.0054 6.817CUGWD11AF D C1 4 1 6.684 0.130 24 BGM / HGM 0.0054 6.567CUGWD11BF D C1 4 1 71.774 0.130 24 HGM 0.0054 70.564CUGWD11DF D C1 4 1 70.355 0.131 24 BGM / HAT 0.0055 70.082CUGWD11EF D C1 4 1 72.456 0.132 24 BGM 0.0055 72.195CUGWD11FF D C1 4 1 68.212 0.131 24 BGM 0.0055 67.831CUGWD217F D C2 4 2 6.793 0.132 24 BGM 0.0055 6.768CUGWD218F D C2 4 2 6.762 0.131 24 BGM 0.0054 6.693CUGWD219F D C2 4 2 6.641 0.130 24 HGM / HIT 0.0054 6.564CUGWD21AF D C2 4 2 67.116 0.130 24 BGM 0.0054 65.915CUGWD21BF D C2 4 2 69.509 0.131 24 HGM 0.0055 69.081CUGWD21CF D C2 4 2 70.047 0.131 24 BGM / HIT 0.0054 69.330CUGWE11JF E C1 5 1 6.754 0.132 24 CIB/CIT/BGM 0.0055 6.778CUGWE11KF E C1 5 1 6.818 0.133 24 BGM 0.0055 6.862CUGWE11LF E C1 5 1 6.999 0.132 24 HGM 0.0055 7.007CUGWE11MF E C1 5 1 6.860 0.133 24 BGM 0.0055 6.912CUGWE11NF E C1 5 1 70.472 0.132 24 BGM / HIT 0.0055 70.346CUGWE11OF E C1 5 1 70.192 0.132 24 HGM 0.0055 70.133CUGWE11PF E C1 5 1 68.718 0.133 24 BGM 0.0056 69.414CUGWE11QF E C1 5 1 68.919 0.131 24 HGM 0.0055 68.652CUGWE11RF E C1 5 1 69.293 0.133 24 BGM 0.0055 69.634CUGWE21HF E C2 5 2 6.915 0.132 24 BGM 0.0055 6.893CUGWE21IF E C2 5 2 6.780 0.131 24 BGM 0.0055 6.752CUGWE21JF E C2 5 2 7.114 0.132 24 BGM 0.0055 7.088CUGWE21KF E C2 5 2 64.524 0.131 24 BGM 0.0055 64.255CUGWE21LF E C2 5 2 65.883 0.131 24 BGM 0.0055 65.552CUGWE21MF E C2 5 2 68.420 0.131 24 BGM 0.0055 68.044CUGWF118F F C1 6 1 6.518 0.132 24 CIT / BGM 0.0055 6.534CUGWF119F F C1 6 1 6.304 0.133 24 BGM 0.0055 6.353CUGWF11AF F C1 6 1 6.634 0.133 24 BGM 0.0055 6.684CUGWF11BF F C1 6 1 6.440 0.133 24 HIB / BGM 0.0055 6.483CUGWF11CF F C1 6 1 63.768 0.133 24 BGM 0.0055 64.263CUGWF11DF F C1 6 1 66.066 0.133 24 BGM 0.0056 66.716CUGWF11EF F C1 6 1 68.378 0.133 24 BGM 0.0056 69.148CUGWF11FF F C1 6 1 69.353 0.133 24 BGM 0.0055 69.799CUGWF217F F C2 6 2 6.718 0.133 24 CIT / CIB / BGM 0.0056 6.788CUGWF218F F C2 6 2 6.840 0.133 24 BGM 0.0056 6.912CUGWF219F F C2 6 2 6.722 0.133 24 BGM / CIT 0.0056 6.797CUGWF21AF F C2 6 2 70.110 0.133 24 BGM / HIB 0.0056 70.893CUGWF21BF F C2 6 2 66.347 0.133 24 HGM 0.0056 66.976CUGWF21CF F C2 6 2 70.734 0.133 24 HGM 0.0055 71.142







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Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGXD111A D C1 4 1 * 5.036 0.104 20 CIB (END CRUSH) / BGM 0.0052 4.738CUGXD112A D C1 4 1 78.152 4.773 0.108 20 BGM 0.0054 76.420 4.667CUGXD113A D C1 4 1 73.521 4.693 0.108 20 BGM 0.0054 71.950 4.593CUGXD114A D C1 4 1 76.166 4.822 0.109 20 BGM 0.0054 75.205 4.761CUGXD115A D C1 4 1 74.924 ** 0.108 20 BGM 0.0054 73.366CUGXD211A D C2 4 2 68.731 5.081 0.103 20 BGM 0.0052 64.583 4.775CUGXD212A D C2 4 2 77.128 4.971 0.109 20 BGM 0.0054 76.146 4.908CUGXD213A D C2 4 2 71.849 4.662 0.109 20 BGM 0.0055 71.441 4.635CUGXE111A E C1 5 1 77.452 5.239 0.102 20 BGM 0.0051 72.153 4.881CUGXE112A E C1 5 1 77.530 4.875 0.109 20 BGM 0.0054 76.605 4.817CUGXE113A E C1 5 1 78.008 4.963 0.109 20 BGM 0.0054 77.006 4.899CUGXE114A E C1 5 1 71.085 4.767 0.109 20 BGM 0.0055 70.706 4.741CUGXE211A E C2 5 2 69.988 5.059 0.107 20 BGM 0.0054 68.334 4.939CUGXE212A E C2 5 2 75.201 4.976 0.109 20 BGM 0.0055 74.842 4.953CUGXE213A E C2 5 2 77.079 4.628 0.110 20 BGM 0.0055 76.746 4.608CUGXF111A F C1 6 1 70.307 5.219 0.102 20 BGM 0.0051 64.882 4.817CUGXF112A F C1 6 1 70.054 4.699 0.111 20 BGM 0.0055 70.452 4.725CUGXF113A F C1 6 1 69.355 4.622 0.111 20 BGM 0.0056 70.143 4.674CUGXF114A F C1 6 1 75.164 4.514 0.111 20 BGM 0.0056 76.044 4.567CUGXF211A F C2 6 2 69.706 4.905 0.104 20 BGM 0.0052 66.039 4.647CUGXF212A F C2 6 2 74.425 4.634 0.111 20 BGM 0.0056 75.119 4.677CUGXF213A F C2 6 2 70.145 4.540 0.111 20 BGM 0.0055 70.751 4.579








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Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGXD117F D C1 4 1 4.051 0.108 20 BGM 0.0054 3.960CUGXD118F D C1 4 1 3.964 0.108 20 BGM 0.0054 3.903CUGXD119F D C1 4 1 3.827 0.109 20 DIT / CIT 0.0055 3.802CUGXD11AF D C1 4 1 3.784 0.108 20 BGM 0.0054 3.729CUGXD11BF D C1 4 1 40.794 0.108 20 BGM 0.0054 40.233CUGXD11CF D C1 4 1 46.121 0.109 20 BGM 0.0054 45.587CUGXD11DF D C1 4 1 47.839 0.108 20 BGM / DGB 0.0054 46.839CUGXD11EF D C1 4 1 46.038 0.109 20 BGM 0.0054 45.557CUGXD218F D C2 4 2 3.944 0.109 20 BGM 0.0054 3.890CUGXD219F D C2 4 2 3.821 0.108 20 BGM 0.0054 3.768CUGXD21AF D C2 4 2 43.177 0.109 20 BGM 0.0054 42.622CUGXD21BF D C2 4 2 44.768 0.109 20 BGM 0.0054 44.208CUGXD21CF D C2 4 2 44.876 0.109 20 BGM 0.0055 44.555CUGXE117F E C1 5 1 3.878 0.109 20 BGM 0.0055 3.858CUGXE118F E C1 5 1 3.924 0.110 20 BGM 0.0055 3.908CUGXE119F E C1 5 1 4.175 0.111 20 BGM 0.0056 4.222CUGXE11AF E C1 5 1 4.061 0.110 20 BGM 0.0055 4.078CUGXE11BF E C1 5 1 43.376 0.109 20 BGM 0.0055 43.154CUGXE11CF E C1 5 1 40.288 0.111 20 BGM 0.0055 40.526CUGXE11DF E C1 5 1 44.625 0.110 20 BGM 0.0055 44.488CUGXE11EF E C1 5 1 41.283 0.110 20 BGM 0.0055 41.396CUGXE217F E C2 5 2 3.949 0.111 20 BGM 0.0055 3.970CUGXE218F E C2 5 2 3.959 0.111 20 BGM 0.0055 3.993CUGXE219F E C2 5 2 4.160 0.111 20 BGM 0.0055 4.179CUGXE21AF E C2 5 2 44.012 0.110 20 BGM 0.0055 44.182CUGXE21BF E C2 5 2 45.025 0.110 20 BGM 0.0055 44.831CUGXE21CF E C2 5 2 47.853 0.111 20 BGM 0.0055 48.163CUGXF117F F C1 6 1 3.844 0.112 20 BGM 0.0056 3.897CUGXF118F F C1 6 1 4.011 0.111 20 BGM 0.0056 4.060CUGXF119F F C1 6 1 3.912 0.111 20 BGM 0.0056 3.956CUGXF11AF F C1 6 1 3.677 0.111 20 BGM 0.0056 3.725CUGXF11BF F C1 6 1 43.155 0.111 20 BGM 0.0056 43.714CUGXF11CF F C1 6 1 43.618 0.111 20 BGM 0.0055 43.827CUGXF11DF F C1 6 1 44.106 0.112 20 BGM 0.0056 44.732CUGXF11EF F C1 6 1 44.249 0.111 20 BGM 0.0056 44.772CUGXF217F F C2 6 2 3.936 0.111 20 BGM 0.0056 3.976CUGXF218F F C2 6 2 3.743 0.111 20 BGM 0.0056 3.781CUGXF219F F C2 6 2 3.928 0.111 20 BGM 0.0056 3.976CUGXF21AF F C2 6 2 42.972 0.112 20 BGM 0.0056 43.739CUGXF21BF F C2 6 2 41.064 0.111 20 BGM 0.0056 41.494CUGXF21CF F C2 6 2 44.030 0.111 20 BGM 0.0056 44.470







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Cure Cycle #

Prepreg Lot #


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Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGYD111A D C1 4 1 142.082 11.573 0.106 20 BGM 0.0053 136.286 11.101CUGYD112A D C1 4 1 129.410 10.902 0.110 20 BGM 0.0055 129.454 10.906CUGYD113A D C1 4 1 129.199 10.493 0.107 20 BGM 0.0054 125.778 10.215CUGYD114A D C1 4 1 134.536 10.740 0.109 20 BGM 0.0054 133.252 10.637CUGYD211A D C2 4 2 * 11.324 0.105 20 HIT 0.0053 10.834CUGYD212A D C2 4 2 * 11.375 0.109 20 HIT 0.0055 11.297CUGYD213A D C2 4 2 127.028 11.051 0.107 20 BGM 0.0054 123.968 10.785CUGYD214A D C2 4 2 132.296 ** 0.108 20 BGM 0.0054 130.431CUGYD215A D C2 4 2 128.591 ** 0.107 20 BGM 0.0054 125.595CUGYE111A E C1 5 1 137.217 11.282 0.109 20 BGM 0.0054 135.455 11.137CUGYE112A E C1 5 1 129.252 11.268 0.111 20 BGM 0.0055 130.118 11.344CUGYE113A E C1 5 1 126.180 11.013 0.109 20 BGM 0.0055 125.549 10.958CUGYE114A E C1 5 1 128.453 11.036 0.110 20 BGM 0.0055 128.949 11.079CUGYE211A E C2 5 2 131.775 11.224 0.107 20 *BGM 0.0054 128.451 10.941CUGYE212A E C2 5 2 132.016 11.194 0.110 20 BGM 0.0055 131.596 11.159CUGYE213A E C2 5 2 124.214 11.103 0.108 20 *BGM 0.0054 121.715 10.879CUGYF111A F C1 6 1 * 10.987 0.106 20 CIB (END CRUSH) 0.0053 10.564CUGYF112A F C1 6 1 133.972 10.831 0.109 20 BGM 0.0055 133.134 10.764CUGYF113A F C1 6 1 134.109 10.959 0.110 20 BGM 0.0055 133.622 10.919CUGYF114A F C1 6 1 123.856 10.757 0.110 20 BGM 0.0055 123.827 10.755CUGYF115A F C1 6 1 129.081 ** 0.109 20 BGM 0.0055 128.450CUGYF211A F C2 6 2 133.011 10.798 0.110 20 BGM 0.0055 132.602 10.765CUGYF212A F C2 6 2 124.536 10.715 0.111 20 BGM 0.0055 125.328 10.783CUGYF213A F C2 6 2 128.721 11.231 0.111 20 BGM 0.0056 129.993 11.342








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Cure Cycle #




Cure Cycle #

Prepreg Lot #


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Specimen Number

Cytec Batch #

Cytec Cure Cycle


[Msi]


[in]

# Plies in Laminate


[ksi]

Modulusnorm

[Msi]

CUGYD118F D C1 4 1 10.817 0.107 20 BGM / HIB 0.0053 10.497CUGYD119F D C1 4 1 10.140 0.108 20 CIT / CIB 0.0054 9.948CUGYD11AF D C1 4 1 10.589 0.109 20 BAB / HIB 0.0054 10.452CUGYD11BF D C1 4 1 10.634 0.108 20 BGM 0.0054 10.416CUGYD11DF D C1 4 1 86.967 0.109 20 HGM 0.0055 86.453CUGYD11FF D C1 4 1 89.305 0.109 20 HIB / HAT 0.0054 88.270CUGYD11GF D C1 4 1 85.961 0.109 20 BGM 0.0055 85.345CUGYD217F D C2 4 2 10.605 0.109 20 HIB 0.0055 10.527CUGYD218F D C2 4 2 10.366 0.108 20 HIB 0.0054 10.219CUGYD219F D C2 4 2 10.326 0.108 20 HIB / HGM 0.0054 10.166CUGYD21BF D C2 4 2 87.204 0.109 20 HIT / BAT 0.0054 86.044CUGYD21CF D C2 4 2 87.027 0.109 20 HIB / BAB 0.0054 85.998CUGYD21DF D C2 4 2 88.828 0.109 20 BGM 0.0054 87.667CUGYE117F E C1 5 1 10.376 0.109 20 BAB / HIB 0.0055 10.328CUGYE118F E C1 5 1 10.493 0.110 20 BAB / HIB 0.0055 10.455CUGYE119F E C1 5 1 10.912 0.110 20 BAB / HIB 0.0055 10.864CUGYE11AF E C1 5 1 10.937 0.111 20 BAB / HIB 0.0055 10.994CUGYE11BF E C1 5 1 85.482 0.110 20 BGM 0.0055 85.171CUGYE11CF E C1 5 1 85.192 0.110 20 BAT / HIT 0.0055 85.540CUGYE11DF E C1 5 1 86.229 0.111 20 BAB / HIB 0.0055 86.689CUGYE11EF E C1 5 1 83.495 0.110 20 BAB / HIB 0.0055 83.191CUGYE217F E C2 5 2 10.437 0.109 20 BGM / HIB 0.0055 10.381CUGYE218F E C2 5 2 10.357 0.109 20 BAB 0.0054 10.233CUGYE219F E C2 5 2 10.484 0.110 20 BAT / HIT 0.0055 10.446CUGYE21AF E C2 5 2 88.901 0.109 20 BAB / HIB 0.0055 88.335CUGYE21BF E C2 5 2 87.122 0.109 20 BAT 0.0054 86.063CUGYE21CF E C2 5 2 82.456 0.110 20 BAB 0.0055 82.166CUGYF117F F C1 6 1 10.584 0.111 20 HGM 0.0055 10.659CUGYF118F F C1 6 1 10.653 0.110 20 BGM / HIB 0.0055 10.622CUGYF119F F C1 6 1 10.224 0.110 20 BGM 0.0055 10.227CUGYF11AF F C1 6 1 10.590 0.110 20 HGM 0.0055 10.606CUGYF11CF F C1 6 1 85.375 0.109 20 BAB / HIB 0.0055 84.948CUGYF11DF F C1 6 1 87.023 0.110 20 BGM 0.0055 87.359CUGYF11EF F C1 6 1 86.696 0.109 20 BAB / HIB 0.0055 86.184CUGYF11FF F C1 6 1 90.281 0.109 20 BAB / HIB 0.0055 89.768CUGYF217F F C2 6 2 10.678 0.112 20 BAB / HIB 0.0056 10.902CUGYF218F F C2 6 2 10.251 0.111 20 BGM / HIB 0.0056 10.380CUGYF219F F C2 6 2 10.242 0.112 20 BGM / HIB 0.0056 10.398CUGYF21AF F C2 6 2 85.122 0.111 20 BAB / HIB 0.0056 86.070CUGYF21BF F C2 6 2 88.503 0.111 20 BAB 0.0055 89.137CUGYF21CF F C2 6 2 88.662 0.112 20 BGM 0.0056 90.033







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4.13 Lamina Short-Beam Strength Properties (SBS)

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[in]

# Plies in Laminate

Avg. tply [in] Failure Mode

CUGQD117B D C1 4 1 18.810 0.238 45 0.0053 ILSCUGQD118B D C1 4 1 19.986 0.239 45 0.0053 ILSCUGQD119B D C1 4 1 18.544 0.241 45 0.0054 ILSCUGQD11AB D C1 4 1 19.250 0.239 45 0.0053 ILSCUGQD216B D C2 4 2 18.890 0.235 45 0.0052 ILSCUGQD217B D C2 4 2 18.476 0.236 45 0.0052 ILS / TENSIONCUGQD218B D C2 4 2 18.210 0.239 45 0.0053 ILSCUGQD219B D C2 4 2 18.455 0.238 45 0.0053 ILS / COMPRESSIONCUGQE11BB E C1 5 1 18.837 0.248 45 0.0055 ILSCUGQE11DB E C1 5 1 18.191 0.245 45 0.0054 ILS / TENSIONCUGQE11EB E C1 5 1 17.936 0.248 45 0.0055 ILSCUGQE11FB E C1 5 1 17.876 0.247 45 0.0055 ILS / TENSION / COMPRESSIONCUGQE21BB E C2 5 2 18.179 0.247 45 0.0055 ILS / TENSIONCUGQE21DB E C2 5 2 18.414 0.248 45 0.0055 ILSCUGQE21EB E C2 5 2 18.142 0.249 45 0.0055 ILSCUGQF119B F C1 6 1 17.257 0.247 45 0.0055 ILSCUGQF11AB F C1 6 1 17.238 0.247 45 0.0055 ILSCUGQF11BB F C1 6 1 16.717 0.248 45 0.0055 ILSCUGQF11DB F C1 6 1 16.566 0.251 45 0.0056 ILSCUGQF21BB F C2 6 2 18.195 0.247 45 0.0055 ILSCUGQF21CB F C2 6 2 16.003 0.238 45 0.0053 ILSCUGQF21DB F C2 6 2 18.098 0.249 45 0.0055 ILSCUGQF21EB F C2 6 2 18.630 0.250 45 0.0056 ILS

Average 18.126 Average 0.0054Standard Dev. 0.895 Standard Dev.

Coeff. of Var. [%] 4.936 Coeff. of Var. [%]Min. 16.003 Min. 0.0052Max. 19.986 Max. 0.0056

Number of Spec. 23 Number of Spec. 23

Short-Beam Strength Properties (SBS)--CTDStrength



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# Plies in Laminate


CUGQD111A D C1 4 1 15.800 0.233 45 0.0052 ILSCUGQD112A D C1 4 1 16.698 0.235 45 0.0052 ILSCUGQD113A D C1 4 1 16.484 0.235 45 0.0052 ILSCUGQD114A D C1 4 1 16.243 0.237 45 0.0053 ILSCUGQD211A D C2 4 2 15.061 0.239 45 0.0053 ILSCUGQD212A D C2 4 2 15.800 0.238 45 0.0053 ILSCUGQD213A D C2 4 2 15.922 0.238 45 0.0053 ILSCUGQE117A E C1 5 1 15.444 0.245 45 0.0054 ILSCUGQE118A E C1 5 1 15.559 0.247 45 0.0055 ILSCUGQE119A E C1 5 1 15.226 0.247 45 0.0055 ILSCUGQE11AA E C1 5 1 15.220 0.248 45 0.0055 ILSCUGQE217A E C2 5 2 16.004 0.247 45 0.0055 ILSCUGQE218A E C2 5 2 15.889 0.248 45 0.0055 ILSCUGQE219A E C2 5 2 16.274 0.248 45 0.0055 ILSCUGQF111A F C1 6 1 15.588 0.248 45 0.0055 ILSCUGQF112A F C1 6 1 15.535 0.251 45 0.0056 ILSCUGQF113A F C1 6 1 14.502 0.247 45 0.0055 ILSCUGQF117A F C1 6 1 14.606 0.248 45 0.0055 ILSCUGQF217A F C2 6 2 14.843 0.249 45 0.0055 ILSCUGQF218A F C2 6 2 15.786 0.249 45 0.0055 ILSCUGQF219A F C2 6 2 15.932 0.249 45 0.0055 ILS




Short-Beam Strength Properties (SBS)--RTDStrength



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# Plies in Laminate


CUGQD11DC D C1 4 1 12.103 0.238 45 0.0053 ILSCUGQD11EC D C1 4 1 11.633 0.240 45 0.0053 ILSCUGQD11FC D C1 4 1 11.848 0.241 45 0.0053 ILSCUGQD11GC D C1 4 1 12.003 0.239 45 0.0053 ILSCUGQD21BC D C2 4 2 11.071 0.237 45 0.0053 ILSCUGQD21CC D C2 4 2 11.747 0.237 45 0.0053 ILSCUGQD21DC D C2 4 2 11.708 0.237 45 0.0053 ILS




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# Plies in Laminate


CUGQD131D D C1 4 1 10.578 0.242 45 0.0054 ILSCUGQD132D D C1 4 1 9.862 0.244 45 0.0054 ILSCUGQD133D D C1 4 1 9.904 0.244 45 0.0054 ILSCUGQD134D D C1 4 1 10.312 0.246 45 0.0055 ILSCUGQD231D D C2 4 2 10.181 0.244 45 0.0054 ILSCUGQD232D D C2 4 2 10.358 0.243 45 0.0054 ILSCUGQD233D D C2 4 2 10.556 0.246 45 0.0055 ILS




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CUGQD11JE D C1 4 1 9.878 0.243 45 0.0054 ILSCUGQD11KE D C1 4 1 9.824 0.245 45 0.0054 ILSCUGQD11LE D C1 4 1 9.826 0.244 45 0.0054 ILSCUGQD11ME D C1 4 1 9.571 0.242 45 0.0054 ILSCUGQD11NE D C1 4 1 9.594 0.243 45 0.0054 ILSCUGQD21HE D C2 4 2 9.552 0.231 45 0.0051 ILSCUGQD21KE D C2 4 2 9.596 0.235 45 0.0052 ILSCUGQD21LE D C2 4 2 9.481 0.239 45 0.0053 ILS




Short-Beam Strength Properties (SBS)--ETD2Strength



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# Plies in Laminate


CUGQD137F D C1 4 1 8.202 0.247 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQD138F D C1 4 1 8.085 0.244 45 0.0054 ILS / INELASTIC DEFORMATIONCUGQD139F D C1 4 1 7.794 0.245 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQD13AF D C1 4 1 7.644 0.246 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQD237F D C2 4 2 7.641 0.244 45 0.0054 ILS / INELASTIC DEFORMATIONCUGQD238F D C2 4 2 7.616 0.247 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQD239F D C2 4 2 7.534 0.246 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQD23AF D C2 4 2 7.549 0.248 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQE11GF E C1 5 1 8.134 0.248 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQE11HF E C1 5 1 7.629 0.248 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQE11JF E C1 5 1 7.934 0.247 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQE11LF E C1 5 1 7.538 0.247 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQE21HF E C2 5 2 7.600 0.249 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQE21IF E C2 5 2 7.660 0.247 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQE21JF E C2 5 2 7.907 0.246 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQF11FF F C1 6 1 7.865 0.247 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQF11GF F C1 6 1 8.015 0.248 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQF11HF F C1 6 1 7.830 0.249 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQF11JF F C1 6 1 7.502 0.245 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQF21GF F C2 6 2 7.327 0.240 45 0.0053 ILS / INELASTIC DEFORMATIONCUGQF21HF F C2 6 2 7.500 0.249 45 0.0055 ILS / INELASTIC DEFORMATIONCUGQF21IF F C2 6 2 7.389 0.249 45 0.0055 ILS / INELASTIC DEFORMATION




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# Plies in Laminate


CUGqD171A D C1 4 1 14.287 0.175 32 0.0055 ILSCUGqD172A D C1 4 1 14.348 0.175 32 0.0055 ILSCUGqD173A D C1 4 1 14.192 0.176 32 0.0055 ILSCUGqD174A D C1 4 1 13.380 0.177 32 0.0055 ILSCUGqD271A D C2 4 2 12.516 0.172 32 0.0054 ILSCUGqD272A D C2 4 2 13.922 0.175 32 0.0055 ILSCUGqD273A D C2 4 2 14.499 0.176 32 0.0055 ILSCUGqE171A E C1 5 1 14.455 0.177 32 0.0055 ILSCUGqE172A E C1 5 1 13.842 0.179 32 0.0056 ILSCUGqE173A E C1 5 1 14.241 0.177 32 0.0055 ILSCUGqE174A E C1 5 1 13.889 0.177 32 0.0055 ILSCUGqE271A E C2 5 2 11.168 0.168 32 0.0053 ILSCUGqE272A E C2 5 2 14.428 0.175 32 0.0055 ILSCUGqE273A E C2 5 2 13.913 0.174 32 0.0054 ILSCUGqF171A F C1 6 1 12.037 0.171 32 0.0053 ILSCUGqF172A F C1 6 1 13.577 0.177 32 0.0055 ILSCUGqF173A F C1 6 1 13.502 0.177 32 0.0055 ILSCUGqF174A F C1 6 1 13.765 0.177 32 0.0055 ILSCUGqF271A F C2 6 2 14.235 0.176 32 0.0055 ILSCUGqF272A F C2 6 2 13.536 0.177 32 0.0055 ILSCUGqF273A F C2 6 2 14.186 0.178 32 0.0056 ILS




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# Plies in Laminate


CUGqD177F D C1 4 1 8.102 0.173 32 0.0054 ILSCUGqD178F D C1 4 1 8.001 0.175 32 0.0055 ILSCUGqD179F D C1 4 1 7.400 0.177 32 0.0055 ILSCUGqD17AF D C1 4 1 7.611 0.175 32 0.0055 ILSCUGqD276F D C2 4 2 7.927 0.175 32 0.0055 ILSCUGqD277F D C2 4 2 7.892 0.175 32 0.0055 ILSCUGqD278F D C2 4 2 7.846 0.174 32 0.0054 ILSCUGqE177F E C1 5 1 7.351 0.177 32 0.0055 ILSCUGqE178F E C1 5 1 6.943 0.175 32 0.0055 ILSCUGqE179F E C1 5 1 7.157 0.175 32 0.0055 ILSCUGqE17AF E C1 5 1 6.999 0.175 32 0.0055 ILSCUGqE276F E C2 5 2 6.981 0.176 32 0.0055 ILSCUGqE277F E C2 5 2 7.031 0.182 32 0.0057 ILSCUGqE278F E C2 5 2 7.343 0.178 32 0.0056 ILSCUGqF177F F C1 6 1 7.251 0.176 32 0.0055 ILSCUGqF178F F C1 6 1 7.269 0.176 32 0.0055 ILSCUGqF179F F C1 6 1 6.987 0.177 32 0.0055 ILSCUGqF17AF F C1 6 1 7.086 0.177 32 0.0055 ILSCUGqF275F F C2 6 2 6.974 0.178 32 0.0055 ILSCUGqF276F F C2 6 2 7.160 0.178 32 0.0056 ILSCUGqF277F F C2 6 2 7.166 0.177 32 0.0055 ILS




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[in]

# Plies in Laminate


[ksi]

CUGDD115B D C1 4 1 47.191 0.087 16 LGM 0.0054 46.744CUGDD116B D C1 4 1 46.876 0.089 16 LGM 0.0056 47.560CUGDD117B D C1 4 1 45.025 0.087 16 LGM 0.0054 44.530CUGDD118B D C1 4 1 47.541 0.087 16 LGM 0.0055 47.235CUGDD214B D C2 4 2 47.604 0.088 16 LGM 0.0055 47.667CUGDD215B D C2 4 2 45.053 0.089 16 LGM 0.0056 45.505CUGDD216B D C2 4 2 44.733 0.089 16 LGM 0.0056 45.309CUGDE116B E C1 5 1 47.021 0.087 16 LGM 0.0054 46.576CUGDE117B E C1 5 1 44.999 0.086 16 LGM 0.0054 44.002CUGDE118B E C1 5 1 43.509 0.087 16 LGM 0.0054 42.940CUGDE119B E C1 5 1 44.384 0.088 16 LGM 0.0055 44.501CUGDE216B E C2 5 2 43.847 0.088 16 LGM 0.0055 43.980CUGDE217B E C2 5 2 45.807 0.088 16 LGM 0.0055 45.556CUGDE218B E C2 5 2 47.619 0.088 16 LGM 0.0055 47.493CUGDF116B F C1 6 1 50.472 0.089 16 LGM 0.0056 51.046CUGDF117B F C1 6 1 52.269 0.088 16 LGM 0.0055 52.517CUGDF118B F C1 6 1 49.990 0.089 16 LGM 0.0056 50.596CUGDF119B F C1 6 1 48.620 0.089 16 LGM 0.0056 49.338CUGDF216B F C2 6 2 49.974 0.089 16 LGM 0.0055 50.400CUGDF217B F C2 6 2 48.475 0.089 16 LGM 0.0056 48.971CUGDF218B F C2 6 2 46.959 0.088 16 LGM 0.0055 46.737




Laminate Open-Hole Tension Properties (OHT1)--CTDStrength



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# Plies in Laminate


[ksi]

CUGDD111A D C1 4 1 48.304 0.088 16 LGM 0.0055 48.478CUGDD112A D C1 4 1 50.431 0.086 16 LGM 0.0054 49.313CUGDD113A D C1 4 1 46.228 0.088 16 LGM 0.0055 46.376CUGDD114A D C1 4 1 46.984 0.088 16 LGM 0.0055 46.815CUGDD211A D C2 4 2 47.717 0.088 16 LGM 0.0055 47.572CUGDD212A D C2 4 2 46.674 0.088 16 LGM 0.0055 46.921CUGDD213A D C2 4 2 47.628 0.088 16 LGM 0.0055 47.691CUGDE111A E C1 5 1 49.819 0.088 16 LGM 0.0055 49.536CUGDE112A E C1 5 1 46.285 0.086 16 LGM 0.0054 45.207CUGDE113A E C1 5 1 50.430 0.087 16 LGM 0.0055 50.020CUGDE114A E C1 5 1 46.052 0.087 16 LGM 0.0055 45.686CUGDE211A E C2 5 2 47.943 0.088 16 LGM 0.0055 47.807CUGDE212A E C2 5 2 48.538 0.089 16 LGM 0.0056 49.099CUGDE213A E C2 5 2 48.077 0.089 16 LGM 0.0056 48.624CUGDF111A F C1 6 1 54.842 0.089 16 LGM 0.0055 55.184CUGDF112A F C1 6 1 51.519 0.089 16 LGM 0.0056 52.212CUGDF113A F C1 6 1 53.085 0.089 16 LGM 0.0055 53.508CUGDF211A F C2 6 2 53.526 0.088 16 LGM 0.0055 53.283CUGDF212A F C2 6 2 52.323 0.088 16 LGM 0.0055 52.471CUGDF213A F C2 6 2 53.133 0.089 16 LGM 0.0056 53.697CUGDF214A F C2 6 2 52.171 0.088 16 LGM 0.0055 52.112




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# Plies in Laminate


[ksi]

CUGDD119D D C1 4 1 47.409 0.089 16 LGM 0.0056 47.992CUGDD11AD D C1 4 1 54.620 0.089 16 LGM 0.0056 55.437CUGDD11BD D C1 4 1 52.276 0.089 16 LGM 0.0056 52.969CUGDD11CD D C1 4 1 51.722 0.088 16 LGM 0.0055 51.584CUGDD217D D C2 4 2 53.797 0.089 16 LGM 0.0055 54.113CUGDD218D D C2 4 2 53.363 0.089 16 LGM 0.0056 53.960CUGDD219D D C2 4 2 53.437 0.089 16 LGM 0.0055 53.842




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# Plies in Laminate


[ksi]

CUGDD11DF D C1 4 1 51.555 0.089 16 LGM 0.0056 52.062CUGDD11EF D C1 4 1 49.405 0.089 16 AGM 0.0055 49.798CUGDD11FF D C1 4 1 55.028 0.089 16 LGM 0.0056 55.528CUGDD11GF D C1 4 1 54.423 0.088 16 AGM 0.0055 54.300CUGDD21CF D C2 4 2 53.493 0.088 16 AGM 0.0055 53.543CUGDD21DF D C2 4 2 55.214 0.089 16 AGM 0.0056 56.093CUGDD21EF D C2 4 2 53.209 0.090 16 AGM 0.0056 54.277CUGDE11BF E C1 5 1 50.444 0.089 16 LGM 0.0055 50.826CUGDE11CF E C1 5 1 51.031 0.088 16 AGM 0.0055 50.886CUGDE11DF E C1 5 1 52.911 0.087 16 LGM 0.0055 52.520CUGDE11EF E C1 5 1 51.336 0.087 16 LGM 0.0055 50.879CUGDE21BF E C2 5 2 52.737 0.088 16 AGM 0.0055 53.017CUGDE21CF E C2 5 2 54.564 0.089 16 AGM 0.0056 55.143CUGDE21DF E C2 5 2 55.643 0.088 16 AGM 0.0055 55.337CUGDF11BF F C1 6 1 54.440 0.089 16 AGM 0.0056 55.048CUGDF11CF F C1 6 1 58.775 0.089 16 AGM 0.0056 59.532CUGDF11DF F C1 6 1 52.915 0.089 16 AGM 0.0055 53.346CUGDF21BF F C2 6 2 53.921 0.089 16 AGM 0.0056 54.442CUGDF21CF F C2 6 2 54.129 0.087 16 AGM 0.0055 53.729CUGDF21DF F C2 6 2 53.424 0.088 16 AGM 0.0055 53.211CUGDF21EF F C2 6 2 53.373 0.088 16 AGM 0.0055 53.656







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[in]

# Plies in Laminate


[ksi]

CUGED116B D C1 4 1 43.380 0.112 20 AGM 0.0056 44.084CUGED117B D C1 4 1 44.003 0.111 20 AGM 0.0055 44.276CUGED118B D C1 4 1 43.432 0.110 20 AGM 0.0055 43.524CUGED119B D C1 4 1 43.956 0.111 20 AGM 0.0056 44.482CUGED216B D C2 4 2 42.970 0.109 20 AGM 0.0055 42.671CUGED217B D C2 4 2 43.812 0.110 20 AGM 0.0055 43.806CUGED218B D C2 4 2 44.510 0.110 20 AGM 0.0055 44.402CUGEE116B E C1 5 1 43.358 0.109 20 AGM 0.0055 43.121CUGEE117B E C1 5 1 43.029 0.111 20 AGM 0.0056 43.550CUGEE118B E C1 5 1 43.000 0.112 20 AGM 0.0056 43.638CUGEE119B E C1 5 1 43.325 0.110 20 AGM 0.0055 43.410CUGEE216B E C2 5 2 43.538 0.112 20 AGM 0.0056 44.158CUGEE217B E C2 5 2 42.856 0.111 20 AGM 0.0055 43.103CUGEE218B E C2 5 2 43.699 0.111 20 AGM 0.0056 44.255CUGEF116B F C1 6 1 44.643 0.111 20 AGM 0.0056 45.075CUGEF117B F C1 6 1 43.354 0.111 20 AGM 0.0056 43.900CUGEF118B F C1 6 1 44.111 0.110 20 AGM 0.0055 44.204CUGEF119B F C1 6 1 44.015 0.113 20 AGM 0.0057 45.222CUGEF216B F C2 6 2 43.945 0.111 20 AGM 0.0056 44.351CUGEF217B F C2 6 2 44.851 0.110 20 AGM 0.0055 45.028CUGEF218B F C2 6 2 44.587 0.111 20 AGM 0.0055 44.905







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[in]

# Plies in Laminate


[ksi]

CUGED111A D C1 4 1 41.612 0.111 20 AGM 0.0056 42.041CUGED112A D C1 4 1 42.270 0.111 20 AGM 0.0055 42.507CUGED113A D C1 4 1 41.746 0.111 20 AGM 0.0056 42.265CUGED114A D C1 4 1 43.439 0.111 20 AGM 0.0055 43.801CUGED211A D C2 4 2 42.423 0.110 20 AGM 0.0055 42.269CUGED212A D C2 4 2 41.627 0.112 20 AGM 0.0056 42.460CUGED213A D C2 4 2 42.934 0.111 20 AGM 0.0056 43.324CUGEE111A E C1 5 1 42.494 0.109 20 AGM 0.0055 42.230CUGEE112A E C1 5 1 41.612 0.110 20 AGM 0.0055 41.744CUGEE113A E C1 5 1 41.805 0.110 20 AGM 0.0055 41.964CUGEE114A E C1 5 1 42.603 0.110 20 AGM 0.0055 42.590CUGEE211A E C2 5 2 42.024 0.109 20 AGM 0.0055 41.642CUGEE212A E C2 5 2 42.757 0.110 20 AGM 0.0055 42.750CUGEE213A E C2 5 2 41.694 0.111 20 AGM 0.0056 42.155CUGEF111A F C1 6 1 41.954 0.111 20 AGM 0.0056 42.336CUGEF112A F C1 6 1 42.335 0.112 20 AGM 0.0056 43.073CUGEF113A F C1 6 1 41.804 0.112 20 AGM 0.0056 42.641CUGEF114A F C1 6 1 41.946 0.112 20 AGM 0.0056 42.633CUGEF212A F C2 6 2 42.747 0.111 20 AGM 0.0055 43.071CUGEF213A F C2 6 2 42.123 0.111 20 AGM 0.0056 42.660CUGEF214A F C2 6 2 42.056 0.113 20 AGM 0.0056 43.082







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[in]

# Plies in Laminate


[ksi]

CUGED11BF D C1 4 1 35.531 0.110 20 AGM 0.0055 35.525CUGED11CF D C1 4 1 35.266 0.111 20 AGM 0.0056 35.726CUGED11DF D C1 4 1 35.055 0.110 20 AGM 0.0055 35.071CUGED11EF D C1 4 1 34.569 0.110 20 AGM 0.0055 34.627CUGED21BF D C2 4 2 35.567 0.110 20 AGM 0.0055 35.546CUGED21CF D C2 4 2 34.834 0.111 20 AGM 0.0055 35.035CUGED21DF D C2 4 2 34.955 0.109 20 AGM 0.0054 34.542CUGEE11BF E C1 5 1 35.390 0.112 20 AGM 0.0056 36.087CUGEE11CF E C1 5 1 34.489 0.111 20 AGM 0.0056 34.824CUGEE11EF E C1 5 1 34.176 0.112 20 AGM 0.0056 34.947CUGEE11FF E C1 5 1 35.449 0.111 20 AGM 0.0055 35.749CUGEE21BF E C2 5 2 35.231 0.111 20 AGM 0.0056 35.604CUGEE21CF E C2 5 2 34.870 0.111 20 AGM 0.0055 35.044CUGEE21DF E C2 5 2 34.529 0.111 20 AGM 0.0056 34.943CUGEF11BF F C1 6 1 34.188 0.113 20 AGM 0.0056 34.986CUGEF11CF F C1 6 1 34.391 0.112 20 AGM 0.0056 35.006CUGEF11DF F C1 6 1 34.139 0.111 20 AGM 0.0056 34.532CUGEF11EF F C1 6 1 34.977 0.112 20 AGM 0.0056 35.470CUGEF21BF F C2 6 2 34.869 0.112 20 AGM 0.0056 35.387CUGEF21CF F C2 6 2 35.727 0.111 20 AGM 0.0055 36.024CUGEF21DF F C2 6 2 34.881 0.111 20 AGM 0.0056 35.320







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[in]

# Plies in Laminate


[ksi]

CUGFD116B D C1 4 1 58.183 0.111 20 LGM 0.0056 58.756CUGFD117B D C1 4 1 63.405 0.110 20 LGM 0.0055 63.463CUGFD118B D C1 4 1 64.831 0.112 20 LGM 0.0056 65.833CUGFD119B D C1 4 1 63.080 0.110 20 LGM 0.0055 62.946CUGFD216B D C2 4 2 61.419 0.111 20 LGM 0.0055 61.921CUGFD217B D C2 4 2 60.022 0.110 20 LGM 0.0055 60.040CUGFD218B D C2 4 2 59.303 0.110 20 LGM 0.0055 59.447CUGFE116B E C1 5 1 58.788 0.111 20 LGM 0.0056 59.403CUGFE117B E C1 5 1 65.344 0.111 20 LGM 0.0056 66.086CUGFE118B E C1 5 1 60.870 0.111 20 LGM 0.0055 61.303CUGFE119B E C1 5 1 64.609 0.111 20 LGM 0.0056 65.471CUGFE216B E C2 5 2 71.167 0.110 20 LGM 0.0055 71.447CUGFE217B E C2 5 2 71.802 0.111 20 LGM 0.0056 72.639CUGFE218B E C2 5 2 68.690 0.111 20 LGM 0.0056 69.554CUGFF116B F C1 6 1 66.463 0.111 20 LGM 0.0056 67.138CUGFF117B F C1 6 1 65.788 0.112 20 LGM 0.0056 66.955CUGFF118B F C1 6 1 59.682 0.112 20 LGM 0.0056 60.541CUGFF119B F C1 6 1 65.192 0.111 20 LGM 0.0055 65.745CUGFF216B F C2 6 2 69.310 0.111 20 LGM 0.0056 70.139CUGFF217B F C2 6 2 68.990 0.112 20 LGM 0.0056 70.296CUGFF218B F C2 6 2 69.351 0.111 20 LGM 0.0056 70.108







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[in]

# Plies in Laminate


[ksi]

CUGFD111A D C1 4 1 72.433 0.109 20 LGM 0.0054 71.544CUGFD112A D C1 4 1 73.012 0.111 20 LGM 0.0056 73.886CUGFD113A D C1 4 1 64.538 0.109 20 LGM 0.0055 63.981CUGFD114A D C1 4 1 69.976 0.111 20 LGM 0.0055 70.432CUGFD211A D C2 4 2 64.017 0.112 20 LGM 0.0056 64.987CUGFD212A D C2 4 2 65.631 0.110 20 LGM 0.0055 65.909CUGFD213A D C2 4 2 65.839 0.111 20 LGM 0.0055 66.248CUGFE112A E C1 5 1 71.562 0.112 20 LGM 0.0056 72.624CUGFE113A E C1 5 1 67.495 0.112 20 LGM 0.0056 68.416CUGFE114A E C1 5 1 70.437 0.111 20 LGM 0.0056 71.333CUGFE115A E C1 5 1 73.395 0.112 20 LGM 0.0056 74.462CUGFE211A E C2 5 2 72.675 0.111 20 LGM 0.0055 73.204CUGFE212A E C2 5 2 71.162 0.111 20 LGM 0.0056 71.862CUGFE213A E C2 5 2 71.329 0.112 20 LGM 0.0056 72.594CUGFF111A F C1 6 1 68.891 0.110 20 LGM 0.0055 68.953CUGFF112A F C1 6 1 67.660 0.113 20 LGM 0.0056 69.301CUGFF113A F C1 6 1 65.708 0.111 20 LGM 0.0056 66.365CUGFF114A F C1 6 1 69.513 0.112 20 LGM 0.0056 70.851CUGFF211A F C2 6 2 74.997 0.111 20 LGM 0.0056 75.804CUGFF212A F C2 6 2 74.015 0.111 20 LGM 0.0055 74.643CUGFF213A F C2 6 2 73.737 0.112 20 LGM 0.0056 75.145







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Specimen Number

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[in]

# Plies in Laminate


[ksi]

CUGFD11BF D C1 4 1 83.449 0.110 20 LGM 0.0055 83.145CUGFD11CF D C1 4 1 86.758 0.112 20 LGM 0.0056 88.178CUGFD11DF D C1 4 1 84.652 0.111 20 LGM 0.0056 85.575CUGFD11EF D C1 4 1 79.014 0.111 20 LGM 0.0056 79.852CUGFD21AF D C2 4 2 84.345 0.112 20 LGM 0.0056 85.866CUGFD21BF D C2 4 2 81.837 0.111 20 LGM 0.0056 82.916CUGFD21CF D C2 4 2 81.899 0.112 20 LGM 0.0056 83.264CUGFE11AF E C1 5 1 85.188 0.112 20 LGM 0.0056 86.608CUGFE11BF E C1 5 1 81.760 0.111 20 LGM 0.0055 82.218CUGFE11DF E C1 5 1 82.608 0.112 20 LGM 0.0056 83.998CUGFE11FF E C1 5 1 88.162 0.111 20 LGM 0.0056 88.990CUGFE21BF E C2 5 2 88.673 0.112 20 LGM 0.0056 90.205CUGFE21CF E C2 5 2 86.949 0.112 20 LGM 0.0056 88.345CUGFE21DF E C2 5 2 87.931 0.110 20 LGM 0.0055 88.277CUGFF11CF F C1 6 1 88.006 0.110 20 LGM 0.0055 88.326CUGFF11DF F C1 6 1 86.948 0.112 20 LGM 0.0056 88.252CUGFF11EF F C1 6 1 85.232 0.111 20 LGM 0.0056 86.369CUGFF11FF F C1 6 1 84.501 0.113 20 LGM 0.0057 86.805CUGFF11GF F C1 6 1 90.573 0.110 20 LGM 0.0055 90.861CUGFF21BF F C2 6 2 87.750 0.111 20 LGM 0.0056 88.680CUGFF21CF F C2 6 2 91.001 0.112 20 LGM 0.0056 92.821CUGFF21DF F C2 6 2 83.934 0.112 20 LGM 0.0056 85.320







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Specimen Number

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Cytec Cure Cycle



[in]

# Plies in Laminate


[ksi]

CUG4D115B D C1 4 1 55.962 0.088 16 LGM 0.0055 56.005CUG4D116B D C1 4 1 53.945 0.089 16 LGM 0.0055 54.262CUG4D117B D C1 4 1 55.748 0.089 16 LGM 0.0056 56.297CUG4D118B D C1 4 1 54.515 0.089 16 LGM 0.0056 55.434CUG4D215B D C2 4 2 54.001 0.089 16 LGM 0.0056 54.502CUG4D216B D C2 4 2 54.919 0.090 16 LGM 0.0056 56.052CUG4D217B D C2 4 2 57.172 0.088 16 LGM 0.0055 56.879CUG4E116B E C1 5 1 52.580 0.089 16 LGM 0.0056 53.337CUG4E117B E C1 5 1 54.058 0.089 16 LGM 0.0055 54.396CUG4E118B E C1 5 1 55.127 0.088 16 LGM 0.0055 55.399CUG4E119B E C1 5 1 54.663 0.088 16 LGM 0.0055 54.922CUG4E216B E C2 5 2 56.299 0.088 16 LGM 0.0055 56.363CUG4E217B E C2 5 2 55.363 0.088 16 LGM 0.0055 55.321CUG4E218B E C2 5 2 52.650 0.089 16 LGM 0.0056 53.328CUG4F116B F C1 6 1 61.089 0.089 16 LGM 0.0056 61.980CUG4F117B F C1 6 1 57.853 0.088 16 LGM 0.0055 57.864CUG4F118B F C1 6 1 56.261 0.088 16 LGM 0.0055 56.421CUG4F119B F C1 6 1 58.933 0.089 16 LGM 0.0055 59.279CUG4F217B F C2 6 2 59.224 0.088 16 LGM 0.0055 59.236CUG4F218B F C2 6 2 60.248 0.087 16 LGM 0.0054 59.552CUG4F21AB F C2 6 2 58.012 0.088 16 LGM 0.0055 57.902




Laminate Filled-Hole Tension Properties (FHT1)--CTDStrength



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Laminate Filled‐Hole Tension Strength [ksi]

Laminate Filled-Hole Tension Properties (FHT1)--CTDNormalized Strength


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[in]

# Plies in Laminate


[ksi]

CUG4D111A D C1 4 1 56.566 0.088 16 LGM 0.0055 56.759CUG4D112A D C1 4 1 54.820 0.087 16 LGM 0.0054 54.176CUG4D113A D C1 4 1 53.895 0.088 16 LGM 0.0055 54.109CUG4D114A D C1 4 1 55.211 0.088 16 LGM 0.0055 55.295CUG4D211A D C2 4 2 58.153 0.088 16 LGM 0.0055 58.076CUG4D212A D C2 4 2 54.534 0.088 16 LGM 0.0055 54.607CUG4D213A D C2 4 2 57.728 0.089 16 LGM 0.0055 58.111CUG4E111A E C1 5 1 56.923 0.089 16 LGM 0.0056 57.440CUG4E112A E C1 5 1 57.058 0.088 16 LGM 0.0055 57.307CUG4E113A E C1 5 1 56.209 0.089 16 LGM 0.0056 57.135CUG4E114A E C1 5 1 57.619 0.088 16 LGM 0.0055 57.542CUG4E211A E C2 5 2 56.014 0.087 16 LGM 0.0054 55.441CUG4E212A E C2 5 2 57.313 0.090 16 LGM 0.0056 58.290CUG4E213A E C2 5 2 57.040 0.089 16 LGM 0.0055 57.407CUG4F111A F C1 6 1 59.853 0.088 16 LGM 0.0055 59.819CUG4F112A F C1 6 1 60.282 0.089 16 LGM 0.0056 61.162CUG4F113A F C1 6 1 59.869 0.088 16 LGM 0.0055 59.880CUG4F114A F C1 6 1 62.265 0.088 16 LGM 0.0055 62.525CUG4F213A F C2 6 2 61.769 0.089 16 LGM 0.0055 62.296CUG4F214A F C2 6 2 59.023 0.088 16 LGM 0.0055 59.045CUG4F215A F C2 6 2 60.482 0.088 16 LGM 0.0055 60.780




Laminate Filled-Hole Tension Properties (FHT1)--RTDStrength



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Laminate Filled-Hole Tension Properties (FHT1)--RTDNormalized Strength


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[in]

# Plies in Laminate


[ksi]

CUG4D119D D C1 4 1 60.730 0.087 16 LGM 0.0054 59.868CUG4D11AD D C1 4 1 61.084 0.087 16 LGM 0.0055 60.552CUG4D11BD D C1 4 1 56.942 0.088 16 LGM 0.0055 56.759CUG4D11CD D C1 4 1 63.030 0.088 16 LGM 0.0055 63.316CUG4D218D D C2 4 2 61.306 0.088 16 LGM 0.0055 61.306CUG4D219D D C2 4 2 62.169 0.089 16 LGM 0.0056 62.957CUG4D21AD D C2 4 2 59.274 0.088 16 LGM 0.0055 59.453




Laminate Filled-Hole Tension Properties (FHT1)--ETW1Strength



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Laminate Filled-Hole Tension Properties (FHT1)--ETW1Normalized Strength


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Cytec Cure Cycle



[in]

# Plies in Laminate


[ksi]

CUG4D11DF D C1 4 1 60.579 0.088 16 LGM 0.0055 60.774CUG4D11EF D C1 4 1 58.250 0.089 16 LGM 0.0055 58.692CUG4D11FF D C1 4 1 60.664 0.088 16 LGM 0.0055 60.607CUG4D11GF D C1 4 1 58.301 0.088 16 MGM 0.0055 58.544CUG4D21CF D C2 4 2 57.914 0.089 16 AGM 0.0056 58.561CUG4D21DF D C2 4 2 60.810 0.087 16 LGM 0.0055 60.315CUG4D21FF D C2 4 2 61.652 0.088 16 MGM 0.0055 61.629CUG4E11BF E C1 5 1 60.779 0.088 16 AGM 0.0055 61.033CUG4E11CF E C1 5 1 60.109 0.088 16 AGM 0.0055 60.393CUG4E11DF E C1 5 1 59.896 0.089 16 AGM 0.0056 60.656CUG4E11EF E C1 5 1 57.298 0.089 16 AGM 0.0056 58.177CUG4E21BF E C2 5 2 58.657 0.090 16 AGM 0.0056 60.012CUG4E21CF E C2 5 2 58.747 0.088 16 AGM 0.0055 58.681CUG4E21DF E C2 5 2 60.709 0.089 16 LGM 0.0056 61.410CUG4F11BF F C1 6 1 59.160 0.089 16 AGM 0.0055 59.519CUG4F11CF F C1 6 1 59.898 0.089 16 AGM 0.0055 60.295CUG4F11DF F C1 6 1 59.235 0.089 16 AGM 0.0055 59.594CUG4F11EF F C1 6 1 61.247 0.089 16 AGM 0.0055 61.781CUG4F21BF F C2 6 2 60.856 0.088 16 AGM 0.0055 61.075CUG4F21CF F C2 6 2 59.995 0.088 16 AGM 0.0055 60.006CUG4F21GF F C2 6 2 58.837 0.089 16 AGM 0.0055 59.249







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Specimen Number

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[in]

# Plies in Laminate


[ksi]

CUG5D116B D C1 4 1 51.283 0.110 20 AGM 0.0055 51.384CUG5D118B D C1 4 1 49.457 0.110 20 AGM 0.0055 49.652CUG5D119B D C1 4 1 50.884 0.109 20 AGM 0.0055 50.444CUG5D11AB D C1 4 1 49.194 0.110 20 AGM 0.0055 49.246CUG5D216B D C2 4 2 51.074 0.110 20 AGM 0.0055 51.190CUG5D217B D C2 4 2 49.935 0.110 20 AGM 0.0055 49.882CUG5D218B D C2 4 2 48.387 0.110 20 AGM 0.0055 48.468CUG5E117B E C1 5 1 50.529 0.111 20 AGM 0.0055 50.804CUG5E118B E C1 5 1 51.218 0.110 20 AGM 0.0055 51.334CUG5E119B E C1 5 1 52.055 0.110 20 AGM 0.0055 52.000CUG5E11AB E C1 5 1 50.109 0.110 20 AGM 0.0055 50.087CUG5E216B E C2 5 2 50.248 0.109 20 AGM 0.0055 49.822CUG5E217B E C2 5 2 51.347 0.110 20 AGM 0.0055 51.534CUG5E219B E C2 5 2 52.305 0.108 20 AGM 0.0054 51.449CUG5F116B F C1 6 1 51.422 0.110 20 AGM 0.0055 51.648CUG5F117B F C1 6 1 52.354 0.111 20 AGM 0.0056 52.957CUG5F118B F C1 6 1 53.569 0.111 20 AGM 0.0056 54.251CUG5F216B F C2 6 2 53.577 0.110 20 AGM 0.0055 53.545CUG5F217B F C2 6 2 53.259 0.110 20 AGM 0.0055 53.089CUG5F218B F C2 6 2 53.727 0.109 20 AGM 0.0054 53.124







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Specimen Number

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Cytec Cure Cycle



[in]

# Plies in Laminate


[ksi]

CUG5D111A D C1 4 1 50.327 0.109 20 AGM 0.0054 49.763CUG5D112A D C1 4 1 52.400 0.109 20 AGM 0.0055 51.963CUG5D113A D C1 4 1 50.312 0.109 20 AGM 0.0055 49.977CUG5D114A D C1 4 1 47.886 0.110 20 AGM 0.0055 47.842CUG5D211A D C2 4 2 46.531 0.111 20 AGM 0.0056 46.954CUG5D212A D C2 4 2 49.329 0.110 20 AGM 0.0055 49.150CUG5D214A D C2 4 2 48.510 0.111 20 AGM 0.0055 48.841CUG5E111A E C1 5 1 48.756 0.110 20 AGM 0.0055 48.556CUG5E113A E C1 5 1 49.341 0.109 20 AGM 0.0055 48.974CUG5E115A E C1 5 1 49.906 0.110 20 AGM 0.0055 49.709CUG5E116A E C1 5 1 49.408 0.109 20 AGM 0.0055 49.041CUG5E212A E C2 5 2 48.545 0.111 20 AGM 0.0056 49.001CUG5E213A E C2 5 2 49.791 0.109 20 AGM 0.0055 49.542CUG5E214A E C2 5 2 47.954 0.111 20 AGM 0.0055 48.216CUG5F111A F C1 6 1 51.529 0.112 20 AGM 0.0056 52.481CUG5F112A F C1 6 1 50.342 0.111 20 AGM 0.0056 50.845CUG5F113A F C1 6 1 51.390 0.111 20 AGM 0.0056 51.919CUG5F211A F C2 6 2 51.137 0.110 20 AGM 0.0055 50.966CUG5F212A F C2 6 2 48.457 0.110 20 AGM 0.0055 48.259CUG5F213A F C2 6 2 49.135 0.110 20 AGM 0.0055 49.165







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Cytec Cure Cycle



[in]

# Plies in Laminate


[ksi]

CUG5D11BF D C1 4 1 40.229 0.109 20 MGM 0.0055 39.937CUG5D11CF D C1 4 1 39.445 0.110 20 MGM 0.0055 39.528CUG5D11DF D C1 4 1 40.050 0.109 20 LGM 0.0055 39.753CUG5D11EF D C1 4 1 39.605 0.109 20 LGM 0.0055 39.383CUG5D21BF D C2 4 2 39.116 0.109 20 MGM 0.0055 38.879CUG5D21CF D C2 4 2 40.227 0.111 20 LGM 0.0055 40.422CUG5D21DF D C2 4 2 40.002 0.109 20 LGM 0.0055 39.760CUG5E11BF E C1 5 1 40.222 0.112 20 MGM 0.0056 40.807CUG5E11CF E C1 5 1 38.994 0.111 20 LGM 0.0055 39.295CUG5E11DF E C1 5 1 39.434 0.111 20 MGM 0.0055 39.715CUG5E11EF E C1 5 1 39.448 0.110 20 MGM 0.0055 39.430CUG5E21CF E C2 5 2 39.889 0.110 20 MGM 0.0055 39.908CUG5E21DF E C2 5 2 40.075 0.111 20 LGM 0.0056 40.482CUG5E21EF E C2 5 2 39.830 0.111 20 LGM 0.0056 40.300CUG5F11BF F C1 6 1 38.135 0.111 20 AGM 0.0055 38.453CUG5F11CF F C1 6 1 39.975 0.111 20 AGM 0.0056 40.471CUG5F11DF F C1 6 1 40.129 0.110 20 AGM 0.0055 40.184CUG5F21BF F C2 6 2 41.201 0.109 20 AGM 0.0055 40.970CUG5F21EF F C2 6 2 41.061 0.109 20 AGM 0.0055 40.806CUG5F21FF F C2 6 2 39.037 0.111 20 AGM 0.0056 39.480







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Cytec Cure Cycle



[in]

# Plies in Laminate


[ksi]

CUG6D116B D C1 4 1 64.801 0.110 20 LGM 0.0055 64.889CUG6D117B D C1 4 1 68.169 0.110 20 LGM 0.0055 67.994CUG6D118B D C1 4 1 65.220 0.110 20 LGM 0.0055 65.062CUG6D119B D C1 4 1 69.991 0.109 20 LGM 0.0054 69.068CUG6D216B D C2 4 2 64.813 0.110 20 LGM 0.0055 65.009CUG6D217B D C2 4 2 68.996 0.109 20 LGM 0.0054 68.055CUG6D218B D C2 4 2 70.287 0.112 20 LGM 0.0056 71.767CUG6E116B E C1 5 1 71.417 0.111 20 LGM 0.0056 72.240CUG6E117B E C1 5 1 68.334 0.112 20 LGM 0.0056 69.349CUG6E118B E C1 5 1 67.685 0.111 20 LGM 0.0055 68.218CUG6E119B E C1 5 1 69.716 0.110 20 LGM 0.0055 69.821CUG6E216B E C2 5 2 69.608 0.111 20 LGM 0.0055 70.093CUG6E218B E C2 5 2 69.349 0.109 20 LGM 0.0055 69.023CUG6E219B E C2 5 2 68.546 0.110 20 LGM 0.0055 68.598CUG6F116B F C1 6 1 68.588 0.113 20 LGM 0.0056 70.324CUG6F117B F C1 6 1 76.406 0.112 20 LGM 0.0056 77.795CUG6F118B F C1 6 1 75.647 0.112 20 LGM 0.0056 76.794CUG6F119B F C1 6 1 69.934 0.112 20 LGM 0.0056 71.068CUG6F216B F C2 6 2 74.870 0.110 20 LGM 0.0055 75.131CUG6F217B F C2 6 2 74.809 0.110 20 LGM 0.0055 74.831CUG6F218B F C2 6 2 76.147 0.110 20 LGM 0.0055 76.470







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[in]

# Plies in Laminate


[ksi]

CUG6D111A D C1 4 1 74.723 0.109 20 LGM 0.0055 74.089CUG6D112A D C1 4 1 78.064 0.110 20 LGM 0.0055 78.147CUG6D114A D C1 4 1 78.777 0.110 20 LGM 0.0055 79.004CUG6D115A D C1 4 1 73.226 0.110 20 LGM 0.0055 73.248CUG6D211A D C2 4 2 78.236 0.109 20 LGM 0.0055 77.679CUG6D212A D C2 4 2 74.447 0.107 20 LGM 0.0054 72.428CUG6D214A D C2 4 2 72.547 0.109 20 LGM 0.0055 71.921CUG6E111A E C1 5 1 75.074 0.110 20 LGM 0.0055 75.369CUG6E112A E C1 5 1 73.965 0.113 20 LGM 0.0056 75.781CUG6E113A E C1 5 1 74.394 0.112 20 LGM 0.0056 75.803CUG6E114A E C1 5 1 72.961 0.110 20 LGM 0.0055 72.994CUG6E211A E C2 5 2 76.686 0.109 20 LGM 0.0055 76.303CUG6E212A E C2 5 2 74.604 0.109 20 LGM 0.0055 74.118CUG6E213A E C2 5 2 76.745 0.109 20 LGM 0.0055 76.129CUG6F111A F C1 6 1 78.963 0.112 20 LGM 0.0056 80.147CUG6F112A F C1 6 1 83.552 0.111 20 LGM 0.0055 84.274CUG6F113A F C1 6 1 77.540 0.112 20 LGM 0.0056 78.773CUG6F114A F C1 6 1 78.990 0.111 20 LGM 0.0056 79.804CUG6F211A F C2 6 2 78.040 0.110 20 LGM 0.0055 78.052CUG6F212A F C2 6 2 82.336 0.110 20 LGM 0.0055 82.011CUG6F214A F C2 6 2 80.213 0.112 20 LGM 0.0056 81.586







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[in]

# Plies in Laminate


[ksi]

CUG6D11BF D C1 4 1 86.500 0.110 20 LGM 0.0055 86.763CUG6D11CF D C1 4 1 84.670 0.112 20 LGM 0.0056 86.030CUG6D11DF D C1 4 1 79.392 0.109 20 LGM 0.0055 79.007CUG6D11EF D C1 4 1 79.018 0.110 20 LGM 0.0055 78.898CUG6D11FF D C1 4 1 83.302 0.110 20 LGM 0.0055 83.075CUG6D21CF D C2 4 2 79.124 0.109 20 LGM 0.0055 78.716CUG6D21DF D C2 4 2 82.332 0.108 20 LGM 0.0054 81.109CUG6D21EF D C2 4 2 78.292 0.111 20 LGM 0.0056 79.087CUG6E11BF E C1 5 1 82.667 0.112 20 LGM 0.0056 84.232CUG6E11CF E C1 5 1 85.985 0.110 20 LGM 0.0055 86.298CUG6E11DF E C1 5 1 82.877 0.111 20 LGM 0.0056 83.932CUG6E11EF E C1 5 1 84.581 0.111 20 LGM 0.0056 85.696CUG6E21BF E C2 5 2 82.531 0.110 20 LGM 0.0055 82.894CUG6E21CF E C2 5 2 87.230 0.109 20 LGM 0.0055 86.648CUG6E21DF E C2 5 2 83.428 0.111 20 LGM 0.0055 83.820CUG6F11BF F C1 6 1 82.207 0.112 20 LGM 0.0056 83.440CUG6F11CF F C1 6 1 82.636 0.112 20 LGM 0.0056 84.238CUG6F11DF F C1 6 1 80.337 0.112 20 LGM 0.0056 81.481CUG6F11EF F C1 6 1 80.616 0.112 20 LGM 0.0056 81.886CUG6F21BF F C2 6 2 79.385 0.111 20 LGM 0.0056 80.167CUG6F21CF F C2 6 2 81.332 0.110 20 LGM 0.0055 81.480CUG6F21DF F C2 6 2 87.168 0.110 20 LGM 0.0055 87.128







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Specimen Number

Cytec Batch #

Cytec Cure Cycle



[in]

# Plies in Laminate


[ksi]

CUGGD111A D C1 4 1 51.412 0.175 32 LGM 0.0055 51.086CUGGD112A D C1 4 1 51.390 0.178 32 LGM 0.0056 51.906CUGGD113A D C1 4 1 52.207 0.177 32 LGM 0.0055 52.360CUGGD114A D C1 4 1 52.081 0.177 32 LGM 0.0055 52.391CUGGD211A D C2 4 2 50.354 0.176 32 LGM 0.0055 50.426CUGGD212A D C2 4 2 49.724 0.176 32 LGM 0.0055 49.629CUGGD213A D C2 4 2 49.213 0.177 32 LGM 0.0055 49.474CUGGE111A E C1 5 1 51.506 0.176 32 LGM 0.0055 51.413CUGGE112A E C1 5 1 51.866 0.178 32 LGM 0.0056 52.538CUGGE113A E C1 5 1 50.148 0.177 32 LGM 0.0055 50.390CUGGE114A E C1 5 1 50.549 0.176 32 LGM 0.0055 50.664CUGGE211A E C2 5 2 49.647 0.176 32 LGM 0.0055 49.676CUGGE214A E C2 5 2 52.028 0.177 32 LGM 0.0055 52.270CUGGE215A E C2 5 2 51.312 0.177 32 LGM 0.0055 51.502CUGGF111A F C1 6 1 50.181 0.176 32 LGM 0.0055 50.310CUGGF112A F C1 6 1 50.664 0.176 32 LGM 0.0055 50.722CUGGF113A F C1 6 1 50.554 0.176 32 LGM 0.0055 50.645CUGGF114A F C1 6 1 49.910 0.177 32 LGM 0.0055 50.056CUGGF211A F C2 6 2 50.407 0.178 32 LGM 0.0056 50.989CUGGF212A F C2 6 2 49.867 0.178 32 LGM 0.0055 50.316CUGGF213A F C2 6 2 49.336 0.178 32 LGM 0.0056 50.004




Laminate Open-Hole Compression Properties (OHC1)--RTDStrength



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Laminate Open‐Hole Compression Strength [ksi]

Laminate Open-Hole Compression Properties (OHC1)--RTDNormalized Strength


Cure Cycle #

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[in]

# Plies in Laminate


[ksi]

CUGGF116D F C1 6 1 44.885 0.177 32 LGM / MGM 0.0055 45.063CUGGF117D F C1 6 1 43.686 0.176 32 LGM 0.0055 43.711CUGGF118D F C1 6 1 44.756 0.177 32 LGM 0.0055 45.056CUGGF119D F C1 6 1 44.501 0.177 32 LGM 0.0055 44.669CUGGF216D F C2 6 2 43.468 0.177 32 LGM 0.0055 43.752CUGGF217D F C2 6 2 44.669 0.176 32 LGM 0.0055 44.707CUGGF218D F C2 6 2 45.159 0.177 32 LGM 0.0055 45.454




Laminate Open-Hole Compression Properties (OHC1)--ETW1Strength



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Laminate Open-Hole Compression Properties (OHC1)--ETW1Normalized Strength


Cure Cycle #

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Specimen Number

Cytec Batch #

Cytec Cure Cycle



[in]

# Plies in Laminate


[ksi]

CUGGD117F D C1 4 1 38.138 0.175 32 LGM 0.0055 38.001CUGGD118F D C1 4 1 37.472 0.179 32 LGM 0.0056 38.164CUGGD119F D C1 4 1 40.436 0.178 32 LGM 0.0056 40.891CUGGD11AF D C1 4 1 40.554 0.177 32 LGM 0.0055 40.811CUGGD216F D C2 4 2 38.563 0.179 32 LGM / MGM 0.0056 39.191CUGGD217F D C2 4 2 37.719 0.177 32 LGM 0.0055 37.912CUGGD218F D C2 4 2 37.479 0.177 32 LGM 0.0055 37.596CUGGE117F E C1 5 1 36.542 0.175 32 LGM 0.0055 36.300CUGGE118F E C1 5 1 39.798 0.178 32 LGM 0.0056 40.250CUGGE119F E C1 5 1 39.532 0.178 32 LGM 0.0056 40.033CUGGE11AF E C1 5 1 38.385 0.177 32 LGM 0.0055 38.537CUGGE216F E C2 5 2 40.242 0.177 32 LGM 0.0055 40.395CUGGE217F E C2 5 2 39.232 0.177 32 LGM 0.0055 39.388CUGGE218F E C2 5 2 41.000 0.177 32 LGM 0.0055 41.327CUGGF11BF F C1 6 1 39.375 0.176 32 LGM 0.0055 39.271CUGGF11CF F C1 6 1 39.931 0.176 32 LGM 0.0055 39.923CUGGF11DF F C1 6 1 38.129 0.176 32 LGM 0.0055 38.122CUGGF11EF F C1 6 1 39.061 0.175 32 LGM 0.0055 38.850CUGGF21BF F C2 6 2 38.771 0.178 32 LGM 0.0056 39.131CUGGF21CF F C2 6 2 39.839 0.177 32 LGM 0.0055 40.039CUGGF21DF F C2 6 2 38.844 0.177 32 LGM 0.0055 39.039







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Specimen Number

Cytec Batch #

Cytec Cure Cycle



[in]

# Plies in Laminate


[ksi]

CUGHD111A D C1 4 1 45.067 0.220 40 AGM 0.0055 44.972CUGHD112A D C1 4 1 46.598 0.221 40 AGM 0.0055 46.845CUGHD113A D C1 4 1 46.005 0.221 40 AGM 0.0055 46.152CUGHD114A D C1 4 1 46.670 0.220 40 AGM / LGM 0.0055 46.733CUGHD211A D C2 4 2 45.890 0.220 40 AGM / LGM 0.0055 45.879CUGHD212A D C2 4 2 47.214 0.220 40 MGM / AGM 0.0055 47.243CUGHD213A D C2 4 2 43.481 0.220 40 MGM / AGM 0.0055 43.431CUGHE111A E C1 5 1 45.496 0.219 40 AGM / LGM 0.0055 45.231CUGHE112A E C1 5 1 43.772 0.223 40 MGM 0.0056 44.296CUGHE113A E C1 5 1 44.518 0.220 40 LGM / AGM 0.0055 44.548CUGHE114A E C1 5 1 45.574 0.221 40 MGM / AGM 0.0055 45.716CUGHE211A E C2 5 2 44.893 0.220 40 MGM / AGM 0.0055 44.828CUGHE212A E C2 5 2 41.692 0.221 40 AGM / MGM 0.0055 41.913CUGHE213A E C2 5 2 41.462 0.220 40 AGM 0.0055 41.415CUGHF111A F C1 6 1 43.321 0.219 40 AGM / MGM 0.0055 43.114CUGHF112A F C1 6 1 43.109 0.219 40 AGM / MGM 0.0055 42.972CUGHF113A F C1 6 1 42.975 0.220 40 MGM 0.0055 43.066CUGHF211A F C2 6 2 44.136 0.222 40 AGM / LGM 0.0055 44.523CUGHF212A F C2 6 2 43.126 0.222 40 AGM / MGM 0.0055 43.475CUGHF213A F C2 6 2 45.032 0.221 40 AGM / LGM 0.0055 45.178CUGHF214A F C2 6 2 42.360 0.221 40 AGM / LGM 0.0055 42.640







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Specimen Number

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Cytec Cure Cycle



[in]

# Plies in Laminate


[ksi]

CUGHD117F D C1 4 1 30.908 0.217 40 LGM 0.0054 30.500CUGHD118F D C1 4 1 32.538 0.222 40 LGM / MGM 0.0056 32.842CUGHD119F D C1 4 1 32.686 0.220 40 LGM / MGM 0.0055 32.698CUGHD11AF D C1 4 1 33.833 0.222 40 LGM / AGM 0.0055 34.082CUGHD216F D C2 4 2 33.130 0.219 40 LGM 0.0055 32.992CUGHD217F D C2 4 2 32.666 0.220 40 LGM / MGM 0.0055 32.666CUGHD218F D C2 4 2 32.370 0.219 40 LGM / MGM 0.0055 32.150CUGHE117F E C1 5 1 31.997 0.221 40 LGM / MGM 0.0055 32.113CUGHE118F E C1 5 1 32.258 0.223 40 LGM / MGM 0.0056 32.693CUGHE119F E C1 5 1 32.468 0.222 40 MGM 0.0056 32.795CUGHE11AF E C1 5 1 32.139 0.221 40 LGM / MGM 0.0055 32.305CUGHE216F E C2 5 2 32.435 0.222 40 LGM / AGM 0.0056 32.744CUGHE217F E C2 5 2 32.865 0.222 40 LGM / MGM 0.0056 33.196CUGHE218F E C2 5 2 32.317 0.222 40 LGM / MGM 0.0055 32.567CUGHF116F F C1 6 1 32.508 0.221 40 LGM / MGM 0.0055 32.624CUGHF117F F C1 6 1 32.235 0.220 40 LGM / MGM 0.0055 32.206CUGHF118F F C1 6 1 31.697 0.221 40 LGM / AGM 0.0055 31.786CUGHF217F F C2 6 2 31.424 0.222 40 LGM / MGM 0.0055 31.705CUGHF218F F C2 6 2 31.742 0.221 40 LGM / MGM 0.0055 31.934CUGHF219F F C2 6 2 31.571 0.222 40 LGM 0.0055 31.827CUGHF21AF F C2 6 2 31.506 0.222 40 LGM / MGM 0.0055 31.752







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Cytec Cure Cycle



[in]

# Plies in Laminate


[ksi]

CUGID111A D C1 4 1 68.737 0.216 40 AGM / LGM 0.0054 67.367CUGID112A D C1 4 1 66.500 0.216 40 AGM / LGM 0.0054 65.427CUGID113A D C1 4 1 65.177 0.217 40 AGM / LGM 0.0054 64.180CUGID114A D C1 4 1 67.820 0.219 40 AGM / LGM 0.0055 67.610CUGID211A D C2 4 2 65.999 0.218 40 AGM / LGM 0.0055 65.409CUGID212A D C2 4 2 64.690 0.216 40 AGM / LGM 0.0054 63.411CUGID213A D C2 4 2 65.001 0.219 40 AGM / LGM 0.0055 64.666CUGIE111A E C1 5 1 66.764 0.218 40 AGM / LGM 0.0054 66.005CUGIE112A E C1 5 1 66.284 0.221 40 AGM / LGM 0.0055 66.721CUGIE113A E C1 5 1 67.255 0.220 40 AGM / LGM 0.0055 67.402CUGIE115A E C1 5 1 65.073 0.222 40 AGM / LGM 0.0056 65.792CUGIE211A E C2 5 2 63.450 0.221 40 AGM / LGM 0.0055 63.801CUGIE212A E C2 5 2 67.093 0.221 40 AGM / LGM 0.0055 67.342CUGIE213A E C2 5 2 67.510 0.221 40 AGM / LGM 0.0055 67.837CUGIE214A E C2 5 2 64.242 0.222 40 AGM / LGM 0.0056 64.870CUGIF111A F C1 6 1 64.978 0.223 40 AGM / LGM 0.0056 65.894CUGIF112A F C1 6 1 64.995 0.223 40 AGM / LGM 0.0056 65.852CUGIF113A F C1 6 1 65.543 0.225 40 AGM / LGM 0.0056 66.958CUGIF114A F C1 6 1 63.863 0.224 40 AGM / LGM 0.0056 65.000CUGIF211A F C2 6 2 66.216 0.220 40 AGM / LGM 0.0055 66.356CUGIF212A F C2 6 2 66.833 0.222 40 AGM / LGM 0.0056 67.471CUGIF213A F C2 6 2 66.427 0.222 40 AGM / LGM 0.0055 66.981







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Cytec Cure Cycle



[in]

# Plies in Laminate


[ksi]

CUGID117F D C1 4 1 54.285 0.217 40 LGM 0.0054 53.446CUGID118F D C1 4 1 51.779 0.218 40 LGM 0.0054 51.250CUGID119F D C1 4 1 51.389 0.217 40 LGM 0.0054 50.649CUGID11AF D C1 4 1 51.859 0.220 40 LGM 0.0055 51.804CUGID216F D C2 4 2 54.052 0.218 40 LGM 0.0055 53.577CUGID217F D C2 4 2 52.631 0.217 40 LGM / MGM 0.0054 51.822CUGID218F D C2 4 2 52.881 0.220 40 LGM 0.0055 52.825CUGIE117F E C1 5 1 51.281 0.218 40 LGM 0.0054 50.749CUGIE118F E C1 5 1 53.841 0.221 40 LGM 0.0055 54.102CUGIE119F E C1 5 1 50.612 0.221 40 LGM 0.0055 50.742CUGIE11AF E C1 5 1 53.284 0.220 40 LGM 0.0055 53.244CUGIE216F E C2 5 2 51.540 0.224 40 LGM 0.0056 52.410CUGIE217F E C2 5 2 53.166 0.222 40 LGM 0.0055 53.545CUGIE218F E C2 5 2 51.550 0.222 40 LGM 0.0056 52.093CUGIF117F F C1 6 1 52.593 0.224 40 LGM 0.0056 53.429CUGIF118F F C1 6 1 54.148 0.224 40 LGM 0.0056 55.157CUGIF119F F C1 6 1 54.039 0.223 40 LGM 0.0056 54.805CUGIF11AF F C1 6 1 55.537 0.224 40 LGM 0.0056 56.555CUGIF216F F C2 6 2 52.610 0.222 40 LGM 0.0055 53.028CUGIF217F F C2 6 2 52.375 0.222 40 LGM 0.0056 52.894CUGIF218F F C2 6 2 49.202 0.223 40 LGM 0.0056 49.810







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Specimen Number

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Cytec Cure Cycle



[in]

# Plies in Laminate


[ksi]

CUG7D111A D C1 4 1 84.715 0.177 32 LGF 0.0055 85.020CUG7D112A D C1 4 1 84.713 0.177 32 LGF 0.0055 85.170CUG7D113A D C1 4 1 81.719 0.176 32 LGF 0.0055 81.889CUG7D114A D C1 4 1 84.954 0.177 32 LGF 0.0055 85.541CUG7D211A D C2 4 2 76.113 0.175 32 LGF 0.0055 75.681CUG7D212A D C2 4 2 81.073 0.176 32 LGF 0.0055 80.942CUG7D213A D C2 4 2 82.700 0.176 32 LGF 0.0055 82.692CUG7E111A E C1 5 1 83.692 0.175 32 LGF 0.0055 83.034CUG7E112A E C1 5 1 78.145 0.177 32 LGF 0.0055 78.397CUG7E113A E C1 5 1 81.506 0.177 32 LGF 0.0055 81.984CUG7E114A E C1 5 1 82.760 0.175 32 LGF 0.0055 82.509CUG7E211A E C2 5 2 82.610 0.176 32 LGF 0.0055 82.782CUG7E212A E C2 5 2 85.174 0.177 32 LGF 0.0055 85.674CUG7E213A E C2 5 2 80.414 0.176 32 LGF 0.0055 80.612CUG7F111A F C1 6 1 78.393 0.178 32 LGF 0.0056 79.209CUG7F112A F C1 6 1 78.070 0.176 32 LGF 0.0055 78.226CUG7F113A F C1 6 1 85.246 0.177 32 LGF 0.0055 85.868CUG7F114A F C1 6 1 82.270 0.177 32 LGF 0.0055 82.808CUG7F211A F C2 6 2 69.941 0.177 32 LGF 0.0055 70.470CUG7F212A F C2 6 2 83.812 0.177 32 LGF 0.0055 84.494CUG7F213A F C2 6 2 79.097 0.177 32 LGF 0.0055 79.763




Laminate Filled-Hole Compression Properties (FHC1)--RTDStrength



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Laminate Filled‐Hole Compression Strength [ksi]

Laminate Filled-Hole Compression Properties (FHC1)--RTDNormalized Strength


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[in]

# Plies in Laminate


[ksi]

CUG7F116D F C1 6 1 68.265 0.177 32 LGF / LGM 0.0055 68.646CUG7F117D F C1 6 1 66.509 0.176 32 LGF / LGM 0.0055 66.414CUG7F118D F C1 6 1 67.006 0.177 32 LGF / LGM 0.0055 67.215CUG7F119D F C1 6 1 67.315 0.177 32 LGF / LGM 0.0055 67.819CUG7F216D F C2 6 2 65.505 0.177 32 LGF / LGM 0.0055 66.007CUG7F217D F C2 6 2 67.967 0.177 32 LGF / LGM 0.0055 68.399CUG7F218D F C2 6 2 65.506 0.176 32 LGF / LGM 0.0055 65.580




Laminate Filled-Hole Compression Properties (FHC1)--ETW1Strength



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[in]

# Plies in Laminate


[ksi]

CUG7D117F D C1 4 1 48.453 0.176 32 LGM 0.0055 48.536CUG7D118F D C1 4 1 54.467 0.177 32 LGM 0.0055 54.674CUG7D119F D C1 4 1 55.307 0.176 32 LGM / LGF 0.0055 55.191CUG7D11AF D C1 4 1 57.405 0.176 32 LGM / LGF 0.0055 57.432CUG7D216F D C2 4 2 51.109 0.176 32 LGF / LGM 0.0055 50.963CUG7D217F D C2 4 2 59.517 0.176 32 LGF / LGM 0.0055 59.523CUG7D218F D C2 4 2 59.628 0.176 32 LGF / LGM 0.0055 59.470CUG7E117F E C1 5 1 59.830 0.176 32 LGF / LGM 0.0055 59.972CUG7E118F E C1 5 1 54.148 0.177 32 LGF / LGM 0.0055 54.506CUG7E119F E C1 5 1 55.931 0.178 32 LGF 0.0056 56.461CUG7E11AF E C1 5 1 55.624 0.178 32 LGF / AGM 0.0056 56.204CUG7E216F E C2 5 2 57.426 0.176 32 LGF / LGM 0.0055 57.344CUG7E217F E C2 5 2 56.194 0.177 32 LGF / LGM 0.0055 56.391CUG7E218F E C2 5 2 58.163 0.177 32 LGF / LGM 0.0055 58.449CUG7F11BF F C1 6 1 57.128 0.176 32 LGF / LGM 0.0055 57.139CUG7F11CF F C1 6 1 53.814 0.176 32 LGF / LGM 0.0055 53.936CUG7F11DF F C1 6 1 56.735 0.176 32 LGF / LGM 0.0055 56.826CUG7F11EF F C1 6 1 58.474 0.177 32 LGF / LGM 0.0055 58.646CUG7F21BF F C2 6 2 52.786 0.177 32 LGF / LGM 0.0055 53.166CUG7F21CF F C2 6 2 52.489 0.178 32 LGF / LGM 0.0055 52.962CUG7F21DF F C2 6 2 52.456 0.178 32 LGM 0.0056 53.112







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[in]

# Plies in Laminate


[ksi]

CUG8D111A D C1 4 1 62.473 0.219 40 LGF 0.0055 62.061CUG8D112A D C1 4 1 64.021 0.222 40 LGF 0.0055 64.462CUG8D113A D C1 4 1 63.714 0.219 40 AGF 0.0055 63.541CUG8D114A D C1 4 1 62.708 0.221 40 AGF 0.0055 62.875CUG8D211A D C2 4 2 65.454 0.221 40 LGF 0.0055 65.707CUG8D212A D C2 4 2 63.141 0.220 40 LGF/AGO 0.0055 63.156CUG8D213A D C2 4 2 62.084 0.220 40 AGF 0.0055 62.079CUG8E111A E C1 5 1 60.330 0.221 40 LGF/AGO 0.0055 60.677CUG8E112A E C1 5 1 60.720 0.221 40 LGF/AGF 0.0055 60.895CUG8E113A E C1 5 1 59.461 0.221 40 MGF 0.0055 59.668CUG8E114A E C1 5 1 62.076 0.220 40 AGF 0.0055 61.982CUG8E211A E C2 5 2 63.509 0.222 40 LGF 0.0055 64.076CUG8E212A E C2 5 2 62.228 0.222 40 LGF/AGF 0.0055 62.690CUG8E213A E C2 5 2 61.420 0.221 40 LGF/AGO 0.0055 61.737CUG8F111A F C1 6 1 60.759 0.220 40 AGF 0.0055 60.768CUG8F112A F C1 6 1 58.194 0.222 40 LGF 0.0056 58.763CUG8F113A F C1 6 1 61.956 0.221 40 AGF 0.0055 62.327CUG8F114A F C1 6 1 63.487 0.223 40 AGF 0.0056 64.266CUG8F211A F C2 6 2 58.352 0.220 40 MGF 0.0055 58.427CUG8F212A F C2 6 2 57.455 0.221 40 AGF 0.0055 57.690CUG8F213A F C2 6 2 62.731 0.222 40 AGF 0.0055 63.178







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[in]

# Plies in Laminate


[ksi]

CUG8D117F D C1 4 1 40.404 0.217 40 LGF / AGM 0.0054 39.893CUG8D118F D C1 4 1 39.143 0.223 40 LGM 0.0056 39.600CUG8D119F D C1 4 1 40.318 0.222 40 LGF / LGM 0.0055 40.602CUG8D11AF D C1 4 1 42.572 0.220 40 AGF / LGM 0.0055 42.556CUG8D216F D C2 4 2 41.719 0.219 40 LGM / AGF 0.0055 41.555CUG8D217F D C2 4 2 43.011 0.221 40 LGM / AGF 0.0055 43.180CUG8D218F D C2 4 2 40.646 0.220 40 LGM / AGF 0.0055 40.578CUG8E117F E C1 5 1 39.228 0.219 40 LGM / AGM 0.0055 39.109CUG8E118F E C1 5 1 39.859 0.222 40 AGF / AGM 0.0055 40.155CUG8E119F E C1 5 1 42.144 0.222 40 AGF / LGM 0.0055 42.511CUG8E11AF E C1 5 1 42.743 0.223 40 LGM 0.0056 43.235CUG8E216F E C2 5 2 44.146 0.223 40 AGF / LGM 0.0056 44.671CUG8E217F E C2 5 2 42.414 0.220 40 LGF / LGM 0.0055 42.443CUG8E218F E C2 5 2 40.946 0.222 40 LGF / LGM 0.0056 41.408CUG8F116F F C1 6 1 40.070 0.222 40 LGM / MGF 0.0055 40.352CUG8F117F F C1 6 1 38.669 0.222 40 LGM / AGF 0.0056 39.055CUG8F119F F C1 6 1 39.515 0.223 40 LGM / AGF 0.0056 39.967CUG8F11AF F C1 6 1 40.123 0.222 40 AGF / LGM 0.0055 40.396CUG8F216F F C2 6 2 40.279 0.223 40 AGM / MGM 0.0056 40.826CUG8F217F F C2 6 2 43.138 0.222 40 LGF / LGM 0.0055 43.461CUG8F218F F C2 6 2 40.541 0.222 40 LGM 0.0056 40.947







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[in]

# Plies in Laminate


[ksi]

CUG9D111A D C1 4 1 92.194 0.220 40 AGO 0.0055 91.991CUG9D112A D C1 4 1 93.483 0.220 40 AGO 0.0055 93.490CUG9D113A D C1 4 1 94.623 0.220 40 AGO 0.0055 94.537CUG9D114A D C1 4 1 91.743 0.221 40 AGO 0.0055 92.049CUG9D211A D C2 4 2 95.613 0.219 40 AGO 0.0055 95.272CUG9D212A D C2 4 2 91.992 0.215 40 AGO 0.0054 89.985CUG9D213A D C2 4 2 96.745 0.221 40 AGO 0.0055 97.236CUG9E111A E C1 5 1 94.178 0.217 40 AGO 0.0054 93.044CUG9E112A E C1 5 1 97.604 0.221 40 AGO 0.0055 98.210CUG9E113A E C1 5 1 94.495 0.222 40 AGO 0.0055 95.175CUG9E114A E C1 5 1 97.715 0.220 40 AGO 0.0055 97.545CUG9E211A E C2 5 2 91.592 0.224 40 AGO 0.0056 93.327CUG9E212A E C2 5 2 92.457 0.221 40 AGO 0.0055 92.856CUG9E213A E C2 5 2 96.432 0.221 40 AGO 0.0055 96.717CUG9F111A F C1 6 1 95.403 0.222 40 AGO 0.0055 96.082CUG9F112A F C1 6 1 95.926 0.222 40 AGO 0.0056 96.922CUG9F113A F C1 6 1 95.620 0.221 40 AGO 0.0055 96.033CUG9F114A F C1 6 1 91.158 0.222 40 AGO 0.0056 91.993CUG9F211A F C2 6 2 86.804 0.222 40 AGO 0.0056 87.732CUG9F212A F C2 6 2 94.173 0.224 40 MGO 0.0056 95.757CUG9F213A F C2 6 2 90.190 0.222 40 AGO 0.0055 90.996







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[in]

# Plies in Laminate


[ksi]

CUG9D117F D C1 4 1 70.848 0.219 40 LGM 0.0055 70.451CUG9D118F D C1 4 1 71.050 0.221 40 LGM 0.0055 71.212CUG9D119F D C1 4 1 76.410 0.219 40 LGM 0.0055 75.982CUG9D11AF D C1 4 1 70.935 0.221 40 LGM 0.0055 71.279CUG9D215F D C2 4 2 76.008 0.218 40 LGF / LGM 0.0055 75.340CUG9D219F D C2 4 2 70.322 0.220 40 LGM 0.0055 70.466CUG9D21AF D C2 4 2 72.106 0.218 40 LGM 0.0054 71.413CUG9E117F E C1 5 1 74.182 0.220 40 LGF 0.0055 74.182CUG9E118F E C1 5 1 70.291 0.221 40 LGF 0.0055 70.706CUG9E119F E C1 5 1 70.012 0.221 40 LGF / LGM 0.0055 70.452CUG9E11AF E C1 5 1 71.899 0.221 40 LGF / LGM 0.0055 72.188CUG9E216F E C2 5 2 69.992 0.222 40 LGF / LGM 0.0055 70.517CUG9E217F E C2 5 2 76.396 0.220 40 LGF / LGM 0.0055 76.286CUG9E218F E C2 5 2 74.393 0.220 40 LGF / LGM 0.0055 74.359CUG9F117F F C1 6 1 65.025 0.223 40 LGF / LGM 0.0056 65.976CUG9F118F F C1 6 1 64.694 0.222 40 LGM 0.0056 65.385CUG9F119F F C1 6 1 65.726 0.224 40 LGM 0.0056 66.856CUG9F11AF F C1 6 1 71.604 0.222 40 LGF / LGM 0.0056 72.336CUG9F215F F C2 6 2 67.479 0.222 40 LGF / LGM 0.0056 68.185CUG9F216F F C2 6 2 68.368 0.222 40 LGM 0.0055 68.901CUG9F217F F C2 6 2 71.036 0.223 40 LGM 0.0056 71.946







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Prepreg Lot # Cure Cycle #Initial Peak

Bearing Strength [ksi]

2% Offset Strength [ksi]

Ultimate Strength [ksi]


[in]

# Plies in Laminate

Comments Avg. tply [in]

Initial Peak Bearing

Strengthnorm

[ksi]

2% Offset Strengthnorm

[ksi]

Ultimate Strengthnorm

[ksi]

CUG1D111A D C1 4 1 137.478 150.969 0.085 16 B1I 0.0053 132.114 145.079CUG1D112A D C1 4 1 142.426 152.791 0.086 16 B1I 0.0053 138.488 148.566CUG1D113A D C1 4 1 140.304 138.900 161.408 0.085 16 B1I 0.0053 135.680 134.323 156.089CUG1D114A D C1 4 1 149.632 148.320 150.933 0.085 16 B1I 0.0053 144.899 143.628 146.160CUG1D211A D C2 4 2 130.606 133.627 152.214 0.085 16 B1I 0.0053 125.560 128.464 146.333CUG1D212A D C2 4 2 135.601 139.222 147.349 0.086 16 B1I 0.0054 132.262 135.795 143.721CUG1D213A D C2 4 2 133.703 139.101 159.219 0.085 16 B1I 0.0053 129.043 134.254 153.671CUG1E111A E C1 5 1 137.387 137.367 152.926 0.086 16 B1I 0.0054 134.264 134.245 149.451CUG1E112A E C1 5 1 143.899 166.797 0.088 16 B1I 0.0055 143.409 166.228CUG1E113A E C1 5 1 142.876 142.100 157.120 0.087 16 B1I 0.0054 141.063 140.297 155.127CUG1E114A E C1 5 1 139.485 140.638 149.805 0.088 16 B1I 0.0055 138.930 140.078 149.210CUG1E211A E C2 5 2 144.099 143.656 162.382 0.085 16 B1I 0.0053 139.323 138.895 157.000CUG1E212A E C2 5 2 132.301 133.145 157.802 0.087 16 B1I 0.0054 130.522 131.354 155.680CUG1E213A E C2 5 2 135.803 138.399 151.834 0.087 16 B1I 0.0054 133.745 136.302 149.534CUG1F111A F C1 6 1 133.986 135.066 152.659 0.084 16 B1I 0.0053 128.174 129.208 146.038CUG1F112A F C1 6 1 141.324 140.490 168.234 0.088 16 B1I 0.0055 140.788 139.958 167.597CUG1F113A F C1 6 1 140.699 142.542 156.645 0.088 16 B1I 0.0055 140.352 142.191 156.259CUG1F114A F C1 6 1 141.338 140.806 154.837 0.088 16 B1I 0.0055 141.605 141.073 155.130CUG1F211A F C2 6 2 136.680 139.017 145.247 0.084 16 B1I 0.0052 130.182 132.409 138.343CUG1F212A F C2 6 2 132.763 138.950 152.442 0.088 16 B1I 0.0055 132.034 138.186 151.605CUG1F213A F C2 6 2 137.194 137.323 149.353 0.086 16 B1I 0.0054 134.362 134.488 146.270

Average 138.099 139.642 154.903 Averagenorm 0.0054 135.155 136.627 151.576Standard Dev. 4.824 3.555 6.028 Standard Dev.norm 5.466 4.488 7.098

Coeff. of Var. [%] 3.493 2.546 3.892 Coeff. of Var. [%]norm 4.044 3.285 4.683Min. 130.606 133.145 145.247 Min. 0.0052 125.560 128.464 138.343Max. 149.632 148.320 168.234 Max. 0.0055 144.899 143.628 167.597

Number of Spec. 18 21 21 Number of Spec. 21 18 21 21

Laminate Single-Shear Bearing Properties (SSB1)--RTDStrength



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Laminate Single‐Shear Bearing Initial Peak Bearing Strength [ksi]

Laminate Single-Shear Bearing Properties (SSB1)--RTDNormalized Initial Peak Bearing Strength


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Laminate Single-Shear Bearing Properties (SSB1)--RTDNormalized 2% Offset Strength


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Laminate Single-Shear Bearing Properties (SSB1)--RTDNormalized Ultimate StrengthCytec 5320-1 T650 Unitape Gr 145 RC 33%

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[in]

# Plies in Laminate



Strengthnorm

[ksi]


[ksi]


[ksi]

CUG1D117D D C1 4 1 115.647 119.090 133.384 0.087 16 B1I 0.0054 114.443 117.850 131.995CUG1D118D D C1 4 1 119.851 116.147 133.474 0.088 16 B1I 0.0055 119.555 115.861 133.145CUG1D119D D C1 4 1 115.260 108.992 128.277 0.087 16 B1I 0.0054 114.169 107.960 127.062CUG1D11AD D C1 4 1 116.802 111.079 130.745 0.088 16 B1I 0.0055 116.227 110.532 130.101CUG1D215D D C2 4 2 113.175 110.097 128.078 0.086 16 B1I 0.0054 110.624 107.615 125.191CUG1D216D D C2 4 2 117.929 117.486 139.116 0.087 16 B1I 0.0054 116.478 116.039 137.403CUG1D217D D C2 4 2 113.079 119.757 129.905 0.086 16 B1I 0.0054 110.938 117.488 127.445




Laminate Single-Shear Bearing Properties (SSB1)--ETW1Strength


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Laminate Single-Shear Bearing Properties (SSB1)--ETW1Normalized Ultimate StrengthCytec 5320-1 T650 Unitape Gr 145 RC 33%

Cure Cycle #

Prepreg Lot #


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[in]

# Plies in Laminate



Strengthnorm

[ksi]


[ksi]


[ksi]

CUG1D11DF D C1 4 1 110.949 106.116 118.874 0.085 16 B1I 0.0053 107.314 102.639 114.979CUG1D11EF D C1 4 1 109.257 108.931 111.633 0.087 16 B1I 0.0054 107.830 107.507 110.175CUG1D11FF D C1 4 1 107.519 102.076 116.299 0.086 16 B1I 0.0054 105.523 100.182 114.141CUG1D11GF D C1 4 1 107.626 107.289 122.547 0.087 16 B1I 0.0055 106.954 106.619 121.781CUG1D219F D C2 4 2 100.512 108.823 116.327 0.088 16 B1I 0.0055 100.132 108.411 115.886CUG1D21AF D C2 4 2 104.812 103.776 109.198 0.089 16 B1I 0.0056 105.865 104.818 110.294CUG1D21BF D C2 4 2 97.457 99.031 109.769 0.088 16 B1I 0.0055 97.402 98.974 109.706CUG1E117F E C1 5 1 103.793 104.116 121.949 0.087 16 B1I 0.0055 103.066 103.386 121.094CUG1E118F E C1 5 1 98.008 104.881 115.971 0.088 16 B1I 0.0055 98.305 105.199 116.322CUG1E119F E C1 5 1 99.177 98.898 108.865 0.089 16 B1I 0.0056 100.341 100.059 110.143CUG1E11AF E C1 5 1 103.064 102.326 107.451 0.089 16 B1I 0.0056 104.724 103.974 109.181CUG1E216F E C2 5 2 101.037 100.849 111.608 0.088 16 B1I 0.0055 100.597 100.410 111.121CUG1E217F E C2 5 2 98.723 103.947 110.411 0.089 16 B1I 0.0055 99.340 104.597 111.101CUG1E218F E C2 5 2 104.003 103.870 112.652 0.088 16 B1I 0.0055 104.574 104.441 113.271CUG1F117F F C1 6 1 98.959 100.211 116.890 0.087 16 B1I 0.0054 97.609 98.844 115.296CUG1F118F F C1 6 1 97.966 104.208 114.844 0.088 16 B1I 0.0055 97.613 103.833 114.430CUG1F119F F C1 6 1 100.056 102.979 109.950 0.088 16 B1I 0.0055 100.511 103.447 110.449CUG1F11AF F C1 6 1 101.336 103.214 115.421 0.088 16 B1I 0.0055 101.739 103.624 115.880CUG1F216F F C2 6 2 94.895 99.669 108.158 0.087 16 B1I 0.0054 93.673 98.385 106.765CUG1F217F F C2 6 2 97.955 96.903 118.544 0.090 16 B1I 0.0056 99.773 98.701 120.744CUG1F218F F C2 6 2 93.585 94.993 116.853 0.089 16 B1I 0.0055 94.401 95.820 117.871







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Strength [ksi]Ultimate

Strength [ksi]


[in]

# Plies in Laminate

Comments Avg. tply [in]2% Offset

Strengthnorm

[ksi]


[ksi]

CUG2D111A D C1 4 1 137.394 145.460 0.1063 20 B1I 0.0053 132.752 140.545CUG2D112A D C1 4 1 141.457 164.475 0.1070 20 B1I 0.0053 137.556 159.939CUG2D113A D C1 4 1 137.426 164.763 0.1062 20 B1I 0.0053 132.678 159.072CUG2D114A D C1 4 1 140.305 169.709 0.1067 20 B1I 0.0053 136.096 164.618CUG2D211A D C2 4 2 135.096 165.855 0.1072 20 B1I 0.0054 131.698 161.684CUG2D212A D C2 4 2 135.170 169.592 0.1083 20 B1I 0.0054 133.040 166.920CUG2D213A D C2 4 2 136.383 170.980 0.1077 20 B1I 0.0054 133.531 167.405CUG2E111A E C1 5 1 123.515 151.169 0.1135 20 B1I 0.0057 127.426 155.956CUG2E112A E C1 5 1 129.142 162.827 0.1107 20 B1I 0.0055 130.003 163.912CUG2E113A E C1 5 1 130.701 160.271 0.1109 20 B1I 0.0055 131.790 161.607CUG2E114A E C1 5 1 130.616 167.049 0.1112 20 B1I 0.0056 132.001 168.821CUG2E211A E C2 5 2 139.040 152.576 0.1076 20 B1I 0.0054 135.985 149.224CUG2E212A E C2 5 2 139.391 154.611 0.1105 20 B1I 0.0055 139.962 155.244CUG2E213A E C2 5 2 136.131 157.130 0.1095 20 B1I 0.0055 135.491 156.392CUG2F111A F C1 6 1 135.404 165.160 0.1101 20 B1I 0.0055 135.568 165.361CUG2F112A F C1 6 1 139.791 170.236 0.1104 20 B1I 0.0055 140.341 170.907CUG2F113A F C1 6 1 138.490 159.752 0.1110 20 B1I 0.0055 139.686 161.132CUG2F114A F C1 6 1 135.397 172.698 0.1105 20 B1I 0.0055 135.951 173.405CUG2F211A F C2 6 2 134.215 162.037 0.1089 20 B1I 0.0054 132.873 160.417CUG2F212A F C2 6 2 137.600 167.565 0.1096 20 B1I 0.0055 137.120 166.981CUG2F213A F C2 6 2 137.907 169.495 0.1100 20 B1I 0.0055 137.949 169.546







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Cytec Cure Cycle

Prepreg Lot # Cure Cycle #2% Offset

Strength [ksi]Ultimate

Strength [ksi]


[in]

# Plies in Laminate

Comments Avg. tply [in]2% Offset

Strengthnorm

[ksi]


[ksi]

CUG2D117F D C1 4 1 102.403 117.734 0.1068 20 B1I 0.0053 99.455 114.344CUG2D118F D C1 4 1 105.975 116.038 0.1089 20 B1I 0.0054 104.947 114.912CUG2D119F D C1 4 1 106.759 122.412 0.1091 20 B1I 0.0055 105.886 121.411CUG2D11AF D C1 4 1 106.354 135.217 0.1091 20 B1I 0.0055 105.484 134.110CUG2D216F D C2 4 2 102.958 128.773 0.1104 20 B1I 0.0055 103.333 129.241CUG2D217F D C2 4 2 99.060 115.616 0.1111 20 B1I 0.0056 100.081 116.807CUG2D218F D C2 4 2 102.021 119.920 0.1093 20 B1I 0.0055 101.326 119.103CUG2E117F E C1 5 1 102.862 120.417 0.1107 20 B1I 0.0055 103.532 121.201CUG2E118F E C1 5 1 98.038 114.038 0.1104 20 B1I 0.0055 98.394 114.452CUG2E119F E C1 5 1 99.089 116.014 0.1106 20 B1I 0.0055 99.615 116.629CUG2E11AF E C1 5 1 96.317 120.534 0.1112 20 B1I 0.0056 97.397 121.885CUG2E216F E C2 5 2 93.443 119.369 0.1101 20 B1I 0.0055 93.513 119.459CUG2E217F E C2 5 2 98.840 125.701 0.1112 20 B1I 0.0056 99.918 127.072CUG2E218F E C2 5 2 95.765 116.804 0.1111 20 B1I 0.0056 96.722 117.972CUG2F117F F C1 6 1 104.688 122.588 0.1082 20 B1I 0.0054 102.959 120.563CUG2F118F F C1 6 1 101.915 117.491 0.1113 20 B1I 0.0056 103.104 118.862CUG2F119F F C1 6 1 101.461 121.458 0.1119 20 B1I 0.0056 103.244 123.593CUG2F11AF F C1 6 1 98.296 118.284 0.1116 20 B1I 0.0056 99.755 120.040CUG2F216F F C2 6 2 101.172 118.060 0.1094 20 B1I 0.0055 100.620 117.416CUG2F217F F C2 6 2 101.336 120.866 0.1105 20 B1I 0.0055 101.797 121.416CUG2F218F F C2 6 2 101.289 116.815 0.1104 20 B1I 0.0055 101.642 117.222







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Specimen Number

Cytec Batch #

Cytec Cure Cycle






[in]

# Plies in Laminate



Strengthnorm

[ksi]


[ksi]


[ksi]

CUG3D111A D C1 4 1 129.900 142.358 156.825 0.1080 20 S1I 0.0054 127.539 139.769 153.973CUG3D112A D C1 4 1 125.877 134.410 137.313 0.1082 20 S1I 0.0054 123.817 132.210 135.066CUG3D113A D C1 4 1 128.941 143.602 151.542 0.1098 20 S1I 0.0055 128.707 143.341 151.266CUG3D114A D C1 4 1 142.425 157.196 0.1098 20 S1I 0.0055 142.123 156.862CUG3D115A D C1 4 1 134.761 142.573 151.355 0.1088 20 S1I 0.0054 133.250 140.974 149.658CUG3D211A D C2 4 2 130.842 140.721 144.268 0.1073 20 S1I 0.0054 127.611 137.245 140.705CUG3D212A D C2 4 2 128.171 132.045 143.169 0.1076 20 S1I 0.0054 125.355 129.144 140.024CUG3D213A D C2 4 2 137.351 146.134 150.740 0.1068 20 B1I 0.0053 133.355 141.883 146.355CUG3E111A E C1 5 1 131.612 147.111 147.383 0.1085 20 S1I 0.0054 129.798 145.082 145.351CUG3E112A E C1 5 1 143.496 153.917 0.1117 20 S1I 0.0056 145.648 156.226CUG3E113A E C1 5 1 130.166 141.082 144.333 0.1112 20 S1I 0.0056 131.546 142.579 145.864CUG3E114A E C1 5 1 132.495 138.133 141.954 0.1109 20 S1I 0.0055 133.599 139.284 143.137CUG3E211A E C2 5 2 136.492 143.484 147.933 0.1074 20 S1I 0.0054 133.286 140.115 144.459CUG3E212A E C2 5 2 132.151 136.081 144.655 0.1089 20 S1I 0.0054 130.869 134.762 143.252CUG3E213A E C2 5 2 132.349 135.829 138.931 0.1087 20 S1I 0.0054 130.724 134.162 137.226CUG3F111A F C1 6 1 132.544 129.821 148.766 0.1100 20 B1I 0.0055 132.524 129.802 148.743CUG3F112A F C1 6 1 127.461 130.539 142.501 0.1121 20 S1I 0.0056 129.837 132.972 145.157CUG3F113A F C1 6 1 132.963 135.256 147.119 0.1111 20 B1I 0.0056 134.312 136.629 148.613CUG3F114A F C1 6 1 135.979 141.426 142.327 0.1109 20 S1I 0.0055 137.112 142.604 143.513CUG3F211A F C2 6 2 122.640 127.473 151.904 0.1083 20 B1I 0.0054 120.707 125.465 149.510CUG3F212A F C2 6 2 126.698 131.202 146.547 0.1084 20 S1I 0.0054 124.836 129.274 144.393CUG3F213A F C2 6 2 123.885 137.619 139.674 0.1090 20 S1I 0.0054 122.722 136.326 138.362







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Laminate Single-Shear Bearing Properties (SSB3)--RTDNormalized Initial Peak Bearing Strength


Cure Cycle #

Prepreg Lot #

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[in]

# Plies in Laminate



Strengthnorm

[ksi]


[ksi]


[ksi]

CUG3D117F D C1 4 1 106.168 101.762 123.670 0.1101 20 B1I 0.0055 106.232 101.823 123.745CUG3D118F D C1 4 1 110.044 121.195 0.1093 20 B1I 0.0055 109.327 120.405CUG3D119F D C1 4 1 109.283 121.943 0.1108 20 B1I 0.0055 110.111 122.867CUG3D11AF D C1 4 1 94.832 110.704 128.867 0.1096 20 B1I 0.0055 94.473 110.285 128.379CUG3D216F D C2 4 2 106.059 106.090 121.725 0.1091 20 B1I 0.0055 105.191 105.222 120.729CUG3D217F D C2 4 2 108.489 106.889 122.369 0.1095 20 B1I 0.0055 107.963 106.370 121.776CUG3D218F D C2 4 2 98.454 97.429 116.833 0.1089 20 B1I 0.0054 97.425 96.410 115.611CUG3E117F E C1 5 1 93.350 96.610 117.092 0.1098 20 B1I 0.0055 93.138 96.390 116.826CUG3E118F E C1 5 1 97.816 95.805 115.546 0.1115 20 B1I 0.0056 99.150 97.112 117.121CUG3E119F E C1 5 1 106.682 115.601 0.1114 20 B1I 0.0056 108.007 117.038CUG3E11AF E C1 5 1 97.483 95.641 109.603 0.1112 20 B1I 0.0056 98.517 96.656 110.766CUG3E216F E C2 5 2 105.640 120.729 0.1093 20 B1I 0.0055 104.968 119.961CUG3E217F E C2 5 2 103.349 100.801 122.038 0.1102 20 B1I 0.0055 103.536 100.984 122.259CUG3E218F E C2 5 2 100.202 98.879 120.897 0.1098 20 B1I 0.0055 99.989 98.669 120.641CUG3F116F F C1 6 1 104.273 102.832 124.558 0.1100 20 B1I 0.0055 104.289 102.848 124.577CUG3F117F F C1 6 1 99.874 99.375 114.710 0.1102 20 B1I 0.0055 100.086 99.585 114.954CUG3F118F F C1 6 1 97.923 97.485 122.263 0.1116 20 B1I 0.0056 99.362 98.918 124.060CUG3F119F F C1 6 1 106.025 122.211 0.1116 20 B1I 0.0056 107.535 123.951CUG3F216F F C2 6 2 99.890 98.041 120.633 0.1114 20 B1I 0.0056 101.116 99.244 122.114CUG3F217F F C2 6 2 95.527 98.869 115.076 0.1117 20 B1I 0.0056 96.959 100.352 116.802CUG3F219F F C2 6 2 99.897 105.337 125.594 0.1107 20 B1I 0.0055 100.502 105.975 126.355







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4.30 Compression After Impact 1 Properties (CAI1)


Specimen Number

Cytec Batch #

Cytec Cure Cycle


Measured Impact

Energy (in-lbf)


[in]

# Plies in Laminate


[ksi]

CUGKD111A D C1 4 1 23.711 261.36 0.17418 32 LDM 0.0054 23.466CUGKD112A D C1 4 1 24.283 264.07 0.17636 32 LDM 0.0055 24.333CUGKD113A D C1 4 1 23.923 264.53 0.17549 32 LDM 0.0055 23.853CUGKD114A D C1 4 1 24.897 266.06 0.17649 32 LDM 0.0055 24.966CUGKD115A D C1 4 1 25.044 265.73 0.17660 32 LDM 0.0055 25.129CUGKD116A D C1 4 1 24.487 264.28 0.17629 32 LDM 0.0055 24.527CUGKD117A D C1 4 1 23.549 264.73 0.17704 32 LDM 0.0055 23.687




Laminate Compression After Impact Properties (CAI1)--RTDStrength



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Laminate Compression After Impact Properties (CAI1)--RTDNormalized Strength


Cure Cycle #

Prepreg Lot #


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4.31 Interlaminar Tension Properties (ILT)

Specimen Number

Cytec Batch #

Cytec Cure Cycle

Prepreg Lot # Cure Cycle #Curved Beam Strength [lb]

Interlaminar Tension

Strength [ksi]


[in]

# Plies in Laminate


CUGMD118B D C1 4 1 281.270 8.110 0.162 30 0.0054 ILTCUGMD119B D C1 4 1 281.814 7.986 0.164 30 0.0055 ILTCUGMD11AB D C1 4 1 244.277 6.959 0.164 30 0.0055 ILTCUGMD11BB D C1 4 1 243.688 6.931 0.164 30 0.0055 ILTCUGMD11CB D C1 4 1 188.327 5.416 0.162 30 0.0054 ILTCUGMD11DB D C1 4 1 225.782 6.614 0.160 30 0.0053 ILTCUGMD11EB D C1 4 1 204.346 5.803 0.164 30 0.0055 ILT




Interlaminar Tension Properties (ILT)--CTDStrength



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Curved Beam Strength Properties (CBS)--CTDMeasured CBS


Cure Cycle #

Prepreg Lot #

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Interlaminar Tension Strength [ksi]

Interlaminar Tension Strength (ILT)--CTDMeasured ILT


Cure Cycle #

Prepreg Lot #


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Specimen Number

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Cytec Cure Cycle



Strength [ksi]


[in]

# Plies in Laminate


CUGMD111A D C1 4 1 213.670 6.106 0.163 30 0.0054 ILTCUGMD112A D C1 4 1 235.787 6.766 0.163 30 0.0054 ILTCUGMD113A D C1 4 1 262.114 7.638 0.161 30 0.0054 ILTCUGMD114A D C1 4 1 261.505 7.696 0.159 30 0.0053 ILTCUGMD115A D C1 4 1 266.717 7.866 0.159 30 0.0053 ILTCUGMD116A D C1 4 1 225.227 7.127 0.150 30 0.0050 ILTCUGMD117A D C1 4 1 293.481 8.597 0.160 30 0.0053 ILT




Interlaminar Tension Properties (ILT)--RTDStrength



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Cure Cycle #

Prepreg Lot #

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Interlaminar Tension Strength (ILT)--RTDMeasured ILT


Cure Cycle #

Prepreg Lot #


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Specimen Number

Cytec Batch #

Cytec Cure Cycle



Strength [ksi]


[in]

# Plies in Laminate


CUGMD11FF D C1 4 1 119.620 3.502 0.167 30 0.0056 ILTCUGMD11GF D C1 4 1 167.951 5.055 0.163 30 0.0054 ILTCUGMD11HF D C1 4 1 164.763 5.016 0.162 30 0.0054 ILTCUGMD11IF D C1 4 1 149.971 4.540 0.162 30 0.0054 ILTCUGMD11JF D C1 4 1 174.475 5.212 0.164 30 0.0055 ILTCUGMD11KF D C1 4 1 146.305 4.444 0.162 30 0.0054 ILTCUGMD11LF D C1 4 1 136.017 4.494 0.151 30 0.0050 ILTCUGMD11MF D C1 4 1 167.852 5.489 0.152 30 0.0051 ILT




Interlaminar Tension Properties (ILT)--ETW2Strength



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Curved Beam Strength Properties (CBS)--ETW2Measured CBS


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Interlaminar Tension Strength (ILT)--ETW2Measured ILT


Cure Cycle #

Prepreg Lot #


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5. Additional Compression After Impact Data

Impactor Diameter: 0.625” Representative of Damage Area:

Damage Area and Dent Depth Summary:

Specimen ID Damage Area (inch2) Dent Depth (inch) CUGKD111A 2.252 0.0765

CUGKD112A 2.424 0.058

CUGKD113A 2.014 0.055

CUGKD114A 2.707 0.0575

CUGKD115A 2.793 0.0615

CUGKD116A 3.085 0.0615

CUGKD117A 3.052 0.0665


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6. Full Stress vs. Strain Curves

6.1 Longitudinal Tension - RTD

312095.369

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Strain (micro in/in)

Longitudinal Tension - RTD - Stress vs Strain


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6.2 Transverse Tension – RTD

10439.456

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Transverse Tension - RTD - Stress vs Strain


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6.3 Transverse Compression – RTD

312095.3695

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Transverse Compression - RTD - Stress vs Strain


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6.4 In-Plane Shear – RTD

8315.865

13643.674

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In-Plane Shear - RTD - Shear Stress vs Shear Strain

Data Plot Slope of Data 0.2% Offset 5% Strain


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6.5 “25/50/25” Unnotched Tension 1 – RTD

98353.315

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"25/50/25" Unnotched Tension 1 - RTD - Stress vs Strain


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6.8 “33/0/67” Unnotched Compression 0 – RTD

96027.974

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"33/0/67" Unnotched Compression 0 - RTD - Stress vs Strain


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"10/80/10" Unnotched Compression - RTD - Stress vs Strain


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128199.735

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7. Fluid Sensitivity Comparison

7.1 Room Temperature Data

a 100 Low lead Fuelb Jet A Fuelc Mil-H-5606 Hydraulic Oil

d Mil-H-83282 Hydraulic Oile Engine Lube Oil Mil-L-7808f Engine Lube Oil Mil-L-23699g Salt Waterh Skydrol LD-4

i 50% Water w/ 50% Skydrolr Distilled Waterj MEK washing fluidk Polypropylene Glycol Deicer

q Isopropyl Alcohol DeicingA Dryt 85% Relative Humidity

Per section 6.1 Test Plan

Fluid Exposure

90 days min @ 70°F ± 10F

90 mins @ 70°F ± 10F

48±4 hrs @ 70°F ± 10F

a 2.518

b 3.643

c *

d 3.551

e 2.019

f ‐2.235

g 8.082

h 3.069

i 8.157

j 1.669

k 3.908

q 2.212

r 11.257

A 0.000

t 13.600

*Data for coupons soaked in Mil-H-5606 Hydraulic Oil tested at RTA is not available because data output files could not be located.

Fluid

16.404

Average Short-Beam Strength With Fluid

(ksi)

18.245

15.419

17.486

17.397

17.196

17.299

16.391

17.452

17.84617.149

15.419

17.846 17.846 15.419

17.84615.838

17.846

17.846

17.213

% Strength Reduction With Respect to RTD

15.419

15.419

15.419

15.419

15.419

15.419

15.419

Worst Case Environment Short-

Beam Strength (ksi) (RTW)

17.846

15.419

17.549 15.41917.846

15.419

15.419

15.419

17.846

17.846

15.419

17.846

17.846

17.846

17.846

17.846

17.846

Same Environment Short-Beam Strength

Without Fluid (ksi) (RTD)

*


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Specimen Number

Cytec Batch #

Cytec Cure Cycle

Prepreg Lot #

FluidStrength

[ksi]


[in]

# Plies in Laminate

Avg. tply [in] Failure Mode Average

CUGQE 131a E C 5 a 16.883 0.109 20 0.0054 ILSCUGQE 132a E C 5 a 17.828 0.109 20 0.0054 ILSCUGQE 133a E C 5 a 16.956 0.109 20 0.0055 ILS 17.397

CUGQE 134a E C 5 a 17.520 0.109 20 0.0054 ILS

CUGQE 135a E C 5 a 17.800 0.110 20 0.0055 ILS

CUGQE 13Fb E C 5 b 17.698 0.112 20 0.0056 ILS

CUGQE 13Gb E C 5 b 16.488 0.109 20 0.0055 ILS

CUGQE 13Hb E C 5 b 17.557 0.111 20 0.0056 ILS 17.196

CUGQE 13Ib E C 5 b 17.376 0.110 20 0.0055 ILS

CUGQE 13Jb E C 5 b 16.863 0.110 20 0.0055 ILS

CUGQE 14Fd E C 5 d 16.902 0.111 20 0.0055 ILS

CUGQE 14Gd E C 5 d 17.602 0.109 20 0.0055 ILS

CUGQE 14Hd E C 5 d 17.001 0.112 20 0.0056 ILS 17.213

CUGQE 14Id E C 5 d 17.768 0.109 20 0.0055 ILS

CUGQE 14Jd E C 5 d 16.791 0.111 20 0.0056 ILS

CUGQE 151e E C 5 e 16.968 0.111 20 0.0055 ILS

CUGQE 152e E C 5 e 17.591 0.110 20 0.0055 ILSCUGQE 153e E C 5 e 18.093 0.109 20 0.0054 ILS 17.486CUGQE 154e E C 5 e 17.277 0.109 20 0.0055 ILSCUGQE 155e E C 5 e 17.501 0.109 20 0.0055 ILSCUGQE 15Ff E C 5 f 18.572 0.110 20 0.0055 ILSCUGQE 15Gf E C 5 f 18.661 0.108 20 0.0054 ILSCUGQE 15Hf E C 5 f 18.038 0.111 20 0.0056 ILS 18.245CUGQE 15If E C 5 f 18.542 0.110 20 0.0055 ILSCUGQE 15Jf E C 5 f 17.414 0.111 20 0.0055 ILSCUGQE 161g E C 5 g 16.689 0.109 20 0.0055 ILSCUGQE 162g E C 5 g 16.405 0.109 20 0.0054 ILSCUGQE 163g E C 5 g 16.083 0.111 20 0.0055 ILS 16.404CUGQE 164g E C 5 g 16.126 0.109 20 0.0054 ILSCUGQE 165g E C 5 g 16.718 0.112 20 0.0056 ILSCUGQE 16Fh E C 5 h 17.475 0.108 20 0.0054 ILSCUGQE 16Gh E C 5 h 17.019 0.109 20 0.0054 ILSCUGQE 16Hh E C 5 h 17.679 0.110 20 0.0055 ILS 17.299CUGQE 16Ih E C 5 h 17.130 0.109 20 0.0054 ILSCUGQE 16Jh E C 5 h 17.190 0.110 20 0.0055 ILS

Data for coupons soaked in Mil-H-5606 Hydraulic Oil tested at RTA is not available because data output files could not be located.

Fluid Sensitivity Screening Short-Beam Strength Properties (FSSBS)--RT Strength



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CUGQE 171i E C 5 i 16.030 0.111 20 0.0055 ILSCUGQE 172i E C 5 i 16.821 0.109 20 0.0054 ILSCUGQE 173i E C 5 i 16.223 0.108 20 0.0054 ILS 16.391CUGQE 174i E C 5 i 16.720 0.109 20 0.0054 ILSCUGQE 175i E C 5 i 16.159 0.109 20 0.0055 ILSCUGQE 181j E C 5 j 17.112 0.111 20 0.0055 ILSCUGQE 182j E C 5 j 17.910 0.110 20 0.0055 ILSCUGQE 183j E C 5 j 17.640 0.109 20 0.0054 ILS 17.549CUGQE 184j E C 5 j 17.223 0.110 20 0.0055 ILSCUGQE 185j E C 5 j 17.858 0.110 20 0.0055 ILSCUGQE 18Fk E C 5 k 17.673 0.110 20 0.0055 ILSCUGQE 18Gk E C 5 k 16.690 0.109 20 0.0055 ILSCUGQE 18Hk E C 5 k 18.175 0.111 20 0.0056 ILS 17.149CUGQE 18Ik E C 5 k 17.200 0.110 20 0.0055 ILSCUGQE 18Jk E C 5 k 16.006 0.111 20 0.0055 ILSCUGQE 191q E C 5 q 17.414 0.111 20 0.0056 ILSCUGQE 192q E C 5 q 17.673 0.110 20 0.0055 ILSCUGQE 193q E C 5 q 17.140 0.109 20 0.0054 ILS 17.452CUGQE 194q E C 5 q 17.823 0.110 20 0.0055 ILSCUGQE 195q E C 5 q 17.209 0.110 20 0.0055 ILSCUGQE 19Fr E C 5 r 16.163 0.111 20 0.0055 ILSCUGQE 19Gr E C 5 r 15.815 0.109 20 0.0055 ILSCUGQE 19Hr E C 5 r 15.884 0.112 20 0.0056 ILS 15.838CUGQE 19Ir E C 5 r 15.956 0.110 20 0.0055 ILSCUGQE 19Jr E C 5 r 15.370 0.111 20 0.0056 ILSCUGQE 1A1A E C 5 A 17.154 0.111 20 0.0055 ILSCUGQE 1A2A E C 5 A 18.428 0.109 20 0.0055 ILSCUGQE 1A3A E C 5 A 18.287 0.109 20 0.0054 ILS 17.846CUGQE 1A4A E C 5 A 18.009 0.110 20 0.0055 ILSCUGQE 1A5A E C 5 A 17.355 0.110 20 0.0055 ILSCUGQE 1AFt E C 5 t 15.251 0.110 20 0.0055 ILSCUGQE 1AGt E C 5 t 15.775 0.109 20 0.0055 ILSCUGQE 1AHt E C 5 t 15.711 0.112 20 0.0056 ILS 15.419CUGQE 1AIt E C 5 t 15.594 0.110 20 0.0055 ILSCUGQE 1AJt E C 5 t 14.767 0.111 20 0.0056 ILS

Average 17.063Standard Dev. 0.860

Coeff. of Var. [%] 5.040Min. 14.767Max. 18.661

Number of Spec. 70


of 317

7.2 Elevated Temperature Test Data

1 100 Low lead Fuel2 Jet A Fuel3 Mil-H-5606 Hydraulic Oil4 Mil-H-83282 Hydraulic Oil5 Engine Lube Oil Mil-L-7808

6 Engine Lube Oil Mil-L-236997 Salt Water8 Skydrol LD-49 50% Water w/ 50% Skydrols Distilled Water

m MEK washing fluidn Polypropylene Glycol Deicerp Isopropyl Alcohol Deicing

C DryD 85% Relative Humidity

90 days min @ 70°F ± 10F

90 mins @ 70°F ± 10F

48±4 hrs @ 70°F ± 10F

Per section 6.1 Test Plan

Fluid Exposure

1 6.019

2 4.170

3 5.560

4 3.419

5 4.949

6 ‐0.993

7 11.974

8 4.593

9 13.716

m 5.294

n 4.639

p 7.023

s 8.235

C 0.000

D 19.303

Average Short-Beam Strength With Fluid

(ksi)

Same Environment Short-Beam Strength

Without Fluid (ksi) (ETD)

14.048

14.048

14.048

14.048

14.048

14.048

14.048

14.048

14.048

14.048

11.336 11.33614.048

12.891

14.048

14.048 11.336

14.048 11.336

13.396

13.061

14.048 11.336

14.048 11.336

12.121

13.304 11.336

11.336

12.366

13.403

11.336

11.336

% Strength Reduction With Respect to ETD

11.336

11.336

13.353

14.187

11.336

11.336

13.267

13.568

11.336

11.336

Fluid

13.202

13.462

Worst Case Environment Short-Beam

Strength (ksi) (ETW)


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Specimen Number

Cytec Batch #

Cytec Cure Cycle

Prepreg Lot #

FluidStrength

[ksi]


[in]

# Plies in Laminate

Avg. tply [in] Failure Mode Average

CUGQE 1381 E C 5 1 12.751 0.109 20 0.0054 ILSCUGQE 1391 E C 5 1 13.655 0.110 20 0.0055 ILSCUGQE 13A1 E C 5 1 13.188 0.111 20 0.0055 ILS 13.202

CUGQE 13B1 E C 5 1 13.317 0.109 20 0.0055 ILS

CUGQE 13C1 E C 5 1 13.101 0.109 20 0.0054 ILS

CUGQE 13M2 E C 5 2 13.696 0.110 20 0.0055 ILS

CUGQE 13N2 E C 5 2 13.319 0.109 20 0.0055 ILS

CUGQE 13O2 E C 5 2 13.526 0.109 20 0.0055 ILS 13.462

CUGQE 13P2 E C 5 2 13.306 0.108 20 0.0054 ILS

CUGQE 13Q2 E C 5 2 13.463 0.109 20 0.0054 ILS

CUGQE 1483 E C 5 3 13.637 0.112 20 0.0056 ILS

CUGQE 1493 E C 5 3 13.042 0.110 20 0.0055 ILS

CUGQE 14A3 E C 5 3 13.832 0.109 20 0.0054 ILS 13.267

CUGQE 14B3 E C 5 3 12.983 0.109 20 0.0055 ILS

CUGQE 14C3 E C 5 3 12.841 0.111 20 0.0055 ILS

CUGQE 14M4 E C 5 4 13.675 0.111 20 0.0055 ILS

CUGQE 14N4 E C 5 4 13.874 0.111 20 0.0055 ILS

CUGQE 14O4 E C 5 4 13.532 0.111 20 0.0055 ILS 13.568

CUGQE 14P4 E C 5 4 13.315 0.109 20 0.0055 ILSCUGQE 14Q4 E C 5 4 13.444 0.109 20 0.0054 ILSCUGQE 1585 E C 5 5 13.736 0.112 20 0.0056 ILSCUGQE 1595 E C 5 5 13.712 0.110 20 0.0055 ILSCUGQE 15A5 E C 5 5 13.234 0.109 20 0.0054 ILS 13.353CUGQE 15B5 E C 5 5 12.800 0.109 20 0.0055 ILSCUGQE 15C5 E C 5 5 13.281 0.111 20 0.0055 ILSCUGQE 15M6 E C 5 6 14.478 0.110 20 0.0055 ILSCUGQE 15N6 E C 5 6 14.071 0.110 20 0.0055 ILSCUGQE 15O6 E C 5 6 14.202 0.110 20 0.0055 ILS 14.187CUGQE 15P6 E C 5 6 13.910 0.109 20 0.0054 ILSCUGQE 15Q6 E C 5 6 14.276 0.108 20 0.0054 ILSCUGQE 1687 E C 5 7 12.221 0.109 20 0.0055 ILSCUGQE 1697 E C 5 7 12.428 0.109 20 0.0055 ILSCUGQE 16A7 E C 5 7 12.508 0.111 20 0.0055 ILS 12.366CUGQE 16B7 E C 5 7 12.604 0.110 20 0.0055 ILSCUGQE 16C7 E C 5 7 12.067 0.111 20 0.0055 ILSCUGQE 16M8 E C 5 8 12.998 0.109 20 0.0054 ILSCUGQE 16N8 E C 5 8 13.942 0.109 20 0.0055 ILSCUGQE 16O8 E C 5 8 13.108 0.111 20 0.0055 ILS 13.403CUGQE 16P8 E C 5 8 13.188 0.111 20 0.0056 ILSCUGQE 16Q8 E C 5 8 13.778 0.110 20 0.0055 ILS

Fluid Sensitivity Screening Short-Beam Strength Properties (FSSBS)--ET Strength



of 317

CUGQE 1789 E C 5 9 11.967 0.112 20 0.0056 ILSCUGQE 1799 E C 5 9 11.776 0.110 20 0.0055 ILSCUGQE 17A9 E C 5 9 12.230 0.109 20 0.0054 ILS 12.121CUGQE 17B9 E C 5 9 12.488 0.110 20 0.0055 ILSCUGQE 17C9 E C 5 9 12.145 0.111 20 0.0056 ILSCUGQE 188m E C 5 m 13.329 0.112 20 0.0056 ILSCUGQE 189m E C 5 m 12.861 0.110 20 0.0055 ILSCUGQE 18Am E C 5 m 13.870 0.109 20 0.0055 ILS 13.304CUGQE 18Bm E C 5 m 13.323 0.110 20 0.0055 ILSCUGQE 18Cm E C 5 m 13.139 0.111 20 0.0055 ILSCUGQE 18Mn E C 5 n 13.500 0.111 20 0.0056 ILSCUGQE 18Nn E C 5 n 13.940 0.110 20 0.0055 ILSCUGQE 18On E C 5 n 12.917 0.110 20 0.0055 ILS 13.396CUGQE 18Pn E C 5 n 13.264 0.109 20 0.0055 ILSCUGQE 18Qn E C 5 n 13.360 0.108 20 0.0054 ILSCUGQE 198p E C 5 p 12.573 0.112 20 0.0056 ILSCUGQE 199p E C 5 p 13.376 0.110 20 0.0055 ILSCUGQE 19Ap E C 5 p 13.284 0.109 20 0.0055 ILS 13.061CUGQE 19Bp E C 5 p 12.859 0.109 20 0.0055 ILSCUGQE 19Cp E C 5 p 13.215 0.111 20 0.0056 ILSCUGQE 19Ms E C 5 s 13.584 0.110 20 0.0055 ILSCUGQE 19Ns E C 5 s 12.935 0.110 20 0.0055 ILSCUGQE 19Os E C 5 s 12.828 0.111 20 0.0055 ILS 12.891CUGQE 19Ps E C 5 s 12.695 0.109 20 0.0055 ILSCUGQE 19Qs E C 5 s 12.414 0.109 20 0.0054 ILSCUGQE 1A8C E C 5 C 14.160 0.112 20 0.0056 ILSCUGQE 1A9C E C 5 C 13.856 0.110 20 0.0055 ILSCUGQE 1AAC E C 5 C 14.108 0.109 20 0.0054 ILS 14.048CUGQE 1ABC E C 5 C 13.646 0.109 20 0.0055 ILSCUGQE 1ACC E C 5 C 14.471 0.111 20 0.0055 ILSCUHQB 1AMD B C 2 D 11.674 0.111 20 0.0055 ILSCUHQB 1AND B C 2 D 11.427 0.110 20 0.0055 ILSCUHQB 1AOD B C 2 D 11.244 0.110 20 0.0055 ILS 11.336CUHQB 1APD B C 2 D 11.211 0.109 20 0.0055 ILSCUHQB 1AQD B C 2 D 11.125 0.109 20 0.0054 ILS

Average 13.131Standard Dev. 0.765

Coeff. of Var. [%] 5.828Min. 11.125Max. 14.478

Number of Spec. 75


of 317

7.3 Load Displacement Curves

0

100

200

300

400

500

600

700

0 0.005 0.01 0.015 0.02 0.025

Load

(lbf)

Displacement (in)

Load vs Displacement Curves for 90 Day RT Specimens

100 Low level AV Fuel

Jet A Fuel

MIL 5606 hyrdaulic

DRY

MIL 83282 hyrdaulic

MIL 7808 Engine Oil

MIL 23699 Engine Oil

Salt Water

SKYDROL LD‐4

50% Water, 50% SKYDROL LD‐4

Distilled Water

One Sample Selected per fluid type

0

50

100

150

200

250

300

350

400

450

500

0 0.005 0.01 0.015 0.02 0.025 0.03 0.035

Load

(lbf)

Displacement (in)

Load vs Displacement Curves for 90 Day (180F) Specimens

100 Low level AV Fuel

Jet A Fuel

MIL 5606 hyrdaulic

DRY

MIL 83282 Hydraulic

MIL 7808 Engine Oil

MIL 23699 Engine Oil

Salt Water

SKYDROL LD‐4

50% Water, 50% SKYDROL LD‐4

Distilled Water



of 317

0

100

200

300

400

500

600

0 0.002 0.004 0.006 0.008 0.01 0.012 0.014 0.016 0.018 0.02

Load

(lbf)

Displacement (in)

Load vs Displacement Curves for 90 min. RT Specimens

MEK Washing Fluid ASTM D740

Polypropylene Glycol Deicer


0

50

100

150

200

250

300

350

400

450

500

0 0.005 0.01 0.015 0.02 0.025

Load

(lbf)

Displacement (in)

Load vs Displacement Curves for 90 min. (180F) Specimens

MEK Washing Fluid ASTM D740

Polypropylene Glycol Deicer



of 317

0

100

200

300

400

500

600

0 0.005 0.01 0.015 0.02 0.025

Load

(lbf)

Displacement (in)

Load vs Displacement Curves, 48hrs ± 4hrs RT Specimens

ISOPROPYL ALCOHOL Deicing Agent


0

50

100

150

200

250

300

350

400

450

0 0.005 0.01 0.015 0.02 0.025

Load

(lbf)

Displacement (in)

Load vs Displacement Curves, 48hrs ± 4hrs (180F) Specimens

ISOPROPYL ALCOHOL Deicing Agent



of 317

0

100

200

300

400

500

600

0 0.005 0.01 0.015 0.02 0.025

Load

(lbf)

Displacement (in)

Load vs Displacement Curves 85% Relative Humidity, RT Specimens

85% Relative Humidity @ RT


0

50

100

150

200

250

300

350

400

0 0.005 0.01 0.015 0.02 0.025 0.03

Load

(lbf)

Displacement (in)

Load vs Displacement Curves 85% Relative Humidity, (180F) Specimens

85% Relative Humidity @50F



of 317

8. Moisture Conditioning Charts

8.1 Longitudinal Tension – Thinnest Panel

0.0

0.2

0.4

0.6

0.8

1.0

1.2

0 5 10 15 20 25 30 35 40 45

% W

eig

ht G

ain

(To

tal)

Time (days)

Cytec 5320-1 C35 Unitape

CU-C35-LT-E-C1


of 317

8.2 Short Beam Strength – Thickest Panel

0.0

0.2

0.4

0.6

0.8

1.0

0 20 40 60 80 100 120

% W

eig

ht G

ain

(To

tal)

Time (days)

Cytec 5320-1 C35 Unitape

CUGQF21

For “wet” mechanical test specimens, the drying procedures may not have completely dried the specimens prior to moisture conditioning, so the total amount of moisture absorbed by the specimens may be higher than those recorded in the moisture gain charts.


of 317

9. DMA Results

Tg [°C] Tg [°F] Tg [°C] Tg [°F]CUG7E 21 - 1 196.84 386.31 214.13 417.43CUG7E 21 - 2 199.39 390.90 214.14 417.45CUGJD 11 - 1 207.63 405.73 225.69 438.24CUGJD 11 - 2 209.06 408.31 227.55 441.59CUGJD 21 - 1 209.73 409.51 234.63 454.33CUGJD 21 - 2 209.35 408.83 229.25 444.65CUGJE 11 - 1 206.37 403.47 225.23 437.41CUGJE 11 - 2 206.67 404.01 224.39 435.90CUGJE 21 - 1 208.39 407.10 228.67 443.61CUGJE 21 - 2 205.80 402.44 226.77 440.19CUGJF 11 - 1 207.42 405.36 226.23 439.21CUGJF 11 - 2 207.79 406.02 225.65 438.17CUGJF 21 - 1 206.77 404.19 226.76 440.17CUGJF 21 - 2 207.70 405.86 226.19 439.14CUGLF 11 - 1 194.35 381.83 209.85 409.73CUGLF 11 - 2 194.17 381.51 210.14 410.25CUGLF 21 - 1 193.98 381.16 209.62 409.32CUGLF 21 - 2 193.46 380.23 209.57 409.23

CUGWD 11 - 1 194.56 382.21 212.25 414.05CUGWD 11 - 2 194.19 381.54 211.89 413.40CUGWD 21 - 1 197.11 386.80 213.13 415.63CUGWD 21 - 2 195.91 384.64 213.11 415.60CUGWE 11 - 1 188.24 370.83 206.52 403.74CUGWE 11 - 2 187.88 370.18 206.96 404.53CUGWF 11 - 1 192.12 377.82 210.87 411.57CUGWF 11 - 2 191.91 377.44 210.85 411.53CUGYD 11 - 1 191.32 376.38 210.55 410.99CUGYD 11 - 2 192.47 378.45 210.78 411.40CUGYD 21 - 1 190.78 375.40 209.11 408.40CUGYD 21 - 2 191.76 377.17 210.22 410.40CUGYE 11 - 1 194.49 382.08 211.12 412.02CUGYE 11 - 2 193.30 379.94 210.87 411.57CUGYE 21 - 1 195.05 383.09 210.65 411.17CUGYE 21 - 2 193.70 380.66 211.15 412.07CUGYF 21 - 1 194.63 382.33 212.11 413.80CUGYF 21 - 2 194.69 382.44 211.73 413.11

Average 389.13 421.65Stdev 12.93 14.74

AverageOnset Storage Modulus

DMA Results SummaryCytec 5320-1 Uni (C35) Gulfstream Aerospace CUGDX XX DMA DRY

AveragePeak of Tangent Delta

Sample #


of 317

Tg [°C] Tg [°F] Tg [°C] Tg [°F]CUG7E 21 - 1 161.37 322.47 172.79 343.02CUG7E 21 - 2 160.87 321.57 173.44 344.19CUGJD 11 - 1 166.47 331.65 178.98 354.16CUGJD 11 - 2 166.55 331.79 178.17 352.71CUGJD 21 - 1 161.55 322.79 174.80 346.64CUGJD 21 - 2 162.17 323.91 174.13 345.43CUGJE 11 - 1 161.97 323.55 174.36 345.85CUGJE 11 - 2 161.97 323.55 173.98 345.16CUGJE 21 - 1 162.57 324.63 175.04 347.07CUGJE 21 - 2 162.64 324.75 175.00 347.00CUGJF 11 - 1 165.97 330.75 178.36 353.05CUGJF 11 - 2 165.47 329.85 177.70 351.86CUGJF 21 - 1 165.92 330.66 177.76 351.97CUGJF 21 - 2 166.04 330.87 177.96 352.33CUGLF 11 - 1 159.85 319.73 170.48 338.86CUGLF 11 - 2 160.34 320.61 171.07 339.93CUGLF 21 - 1 159.20 318.56 169.57 337.23CUGLF 21 - 2 159.01 318.22 170.08 338.14

CUGWD 11 - 1 159.32 318.78 173.23 343.81

CUGWD 11 - 2 160.18 320.32 173.18 343.72CUGWD 21 - 1 159.67 319.41 173.11 343.60CUGWD 21 - 2 160.07 320.13 173.01 343.42CUGWE 11 - 1 158.64 317.55 171.51 340.72CUGWE 11 - 2 159.35 318.83 172.16 341.89CUGWF 11 - 1 158.96 318.13 172.84 343.11CUGWF 11 - 2 159.20 318.56 172.50 342.50CUGYD 11 - 1 160.02 320.04 171.84 341.31CUGYD 11 - 2 158.83 317.89 171.71 341.08CUGYD 21 - 1 158.80 317.84 170.73 339.31CUGYD 21 - 2 158.69 317.64 170.77 339.39CUGYE 11 - 1 158.89 318.00 169.85 337.73CUGYE 11 - 2 158.26 316.87 170.29 338.52CUGYE 21 - 1 158.48 317.26 169.94 337.89CUGYE 21 - 2 158.77 317.79 170.30 338.54CUGYF 21 - 1 158.83 317.89 170.71 339.28CUGYF 21 - 2 159.16 318.49 170.78 339.40

Average 321.79 343.73Stdev 4.77 4.99

DMA Results SummaryCytec 5320-1 uni (C35) Gulfstream Aerospace CUGDX XX DMA WET

Sample #Onset Storage Modulus Peak of Tangent Delta

Average Average


of 317

9.1 DMA Dry Batch A


of 317

9.2 DMA Wet Batch A

10. Deviations

1. Fluid Sensitivity Screening:

a. Jet A fuel was used instead of SAE AMS 2629 Jet Reference Fluid.

b. MIL-H-5606 Hydraulic Oil at RTA is not available.

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